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  • 8/18/2019 ULTIMATE STRENGTH OF REINFORCED CONCRETE IN AMERICAN DESIGN PRACTICE

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    PORTLAND CEMENT ASSOCIATION

    RESEARCH AND DEVELOPMENT LABORATORIES

    ULTIMATE STRENGTH OF

    REINFORCED

    CONCRETE IN

    AMERICAN DESIGN PRACTICE

    By Eivind Hognestad

    Authorized Reprint From

    Proceedings of a Symposium on the Strength of

    Concrete Structures, London, May, 1956

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    Bulletins Published by the

    Development Department

    Research and Development Division

    d the

    Portland Cement Association

    D1

    —“Influence of Soil Volume Change and Vegetation on Highway Engf.

    neering,”

    by E, J.

    FELT.

    Reprinted from Twent Sixth Annuat Highuxw Conference of the Universit?j

    of Coiorado, May 12S2.

    D2 -“Nature of Bond in Pre-Tensioned Prestressed Concrete,”

    by

    JACK R.

    J ANNEY,

    Reprinted from JournfIl of the American Concrete Institute (May, 1954);

    proceedings, 30, 717 (12S4).

    D2A—Discussion of the papw “Nature of Bond in Pre-Tensioned Prestressed

    Concrete,”

    by P. W.

    ABELES, K. HAJNAL-KONYI, N. W. HANSON

    and

    Author, JACK R. JANNEY.

    Reprinted from Journal of the American Concrete Institute (December,

    Part 2, 1954): Proceedings, SO, 73S-1 (1254).

    D3

    _f ~Investigationof M~isture.Vo]ume Stability of Concrete Masonry

    Units,” by

    JOSEPH

    J. SRJDELER,March, 1955.

    D4

    —“A Method for Determining the Moisture Condition of Hardened Con-

    crete in Terms of Relative Humidity,”

    by

    CARL A. MENZEL.

    ~le ~ted froml Proceedings, American Soctetv For Testing M@tU’iaiS, 55

    D5 —“Factors Influencing Physical Properties of Soil-Cement Mixtures,”

    by EARL J.

    FELT.

    Reprinted from~ Bulletin 108 of the IIigfwav Research Board, p.

    123 19S5).

    D6 -“Concrete Stress Distribution in Ultimate Strength Design,” by E.

    HOONESTAO, N. W. HANSON and D. MCHENRY.

    Reprinted from JonrnaI of the American Concrete Institute (December,

    1955); Proceedings, 52, 455 (19S6).

    D?

    -“Ultimate Flexural Strength of Prestressed and Conventionally

    Rein-

    forced Concrete Beams,” by J. It. JANNEY, E. HOONESTAD and D. Mc-

    HENRY.

    Reprinted from Journal of the American Concrete Institite (FebruaxT, 19S0;

    Proceedings, S2, S01 (12SS).

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    SYMPOSIUM ON THE STRENGTH OF CONCRETE STRUCTURES

    LONDON MAY 1956

    Sessicm E: Paper 1

    ULTIMATE STRENGTH OF

    REIN FORCE(D CONCRETE IN

    AMERICAN IDESIGN PRACTICE

    by Eivind Hognestad,

    Dr. techn.

    Portland Cement Association, U.S.A.

    SUMJ4AR Y

    Ultimate strength design procedures for reinforced concrete were recom-

    mended in an October 1955 report of a joint committee of the American

    Society of Civil Engineers and the American Concrete Institute. This paper

    discusses the background for and contents of that report, which represents

    a signj?cant stage in the development of an American design practice based

    on ultimate strength by inelastic action.

    Introduction

    The past fifty years have been a period of rapid growth and develop-

    ment in the use of reinforced concrete as a structural material throughout

    the world. The production of Portland cement in the United States rose

    twenty-five fold from about 2 million long tons in 1900 to over 50 million

    tons in 1955. Similarly, the U.S. production of reinforcing stee[ increased

    from a small amount to about 1”8 million tons.

    Introduction of new design procedures for reinforced concrete must be

    considered with this background of great progress and expansion. Though

    the classical straight-line theor:y was evolved when reinforced concrete was

    in its infancy some 60 years ago, it has served us well; and it certainly

    cannot be put aside on the basis that it has led to unreasonable or unsafe

    designs.

    On the other hand, through half a century of practical experience and

    laboratory experimentation, our knowledge regarding the strength and

    behaviour of structural concrete has been vastly improved. To some extent,

    such improvements of knowledge have been utilized in design practice by

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    periodic adjustments and modifications of the straight-line theory. In this

    manner the original sitnplicity of an elastic theory based on a few funda-

    mental assumptions has largely been lost.

    It is primarily to facilitate further progress, therefore, that many of us

    feel that the time has come to introduce a new theory of reinforced con-

    crete design based on the actual inelastic properties of concrete and steel.

    Such a new theory is needed to realize the full future benefits of such

    highly important developments in the field of structural concrete as high-

    strength reinforcement,, prestressing, and precasting.

    DEFINITIONS

    In recent years good progress has been made in the development of

    knowledge regarding the properties of all engineering materials. New and

    improved concepts of structural behaviour and design have therefore

    become significant in the practice of civil engineering. These concepts are

    identified by rather reeent additions to engineering terminology such as

    rheology, plasticity, inelastic behaviour, plastic analysis, limit strength,

    and many others. Definitions for these terms vary to some extent between

    countries as well as between groups concerned with the various materials.

    It is necessary, therefore, to define common American word usage in

    connexion with structural concrete design.

    Ultimate strenglh design

    Ultimate strength design indicates a method of structural design based

    on the ultimate strength by inelastic action of conventionally reinforced or

    prestressed structural concrete cross-sections subject to simple bending,

    axial load, shear, bond., or combinations thereof. Ultima~e strength design

    does not necessarily involve an inelastic theory of structures. Evaluation

    of external moments and forces that act in indeterminate structural frame-

    works by virtue of dead and live loads may be carried out either by the

    theory of elastic displacements or by limit design.

    Limit design

    Limit design indicates a design method involving an inelastic theory of

    structures in which readjustments in the relative magnitude of bending

    moments at various sections due to non-linear relationships between loads

    and moments at high loads are recognized. Limit design does not by

    definition necessarily involve a final design of sections on an inelastic

    basis.

    Yield line theory

    Yield line theory indicates a theory of reinforced concrete slab structures

    based on inelastic behaviour occurring in a pattern of yield lines, the

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    location of which depends on loading and boundary conditions. Final

    design of sections does not necessarily involve inelastic action.

    So far, most American work regarding inelastic behaviour of structural

    concrete has been devoted to ultimate strength design. A term indicating

    ,a combination of ultimate strength design, limit design and yield line

    theory therefore still remains tc}be adopted. Perhaps the most important

    aspect of ultimate strength design is that it represents a significant step

    toward a broader consideration of inelastic behaviour in design.

    AMERICAN DESIGN SPECIFICATIONS

    Two groups have made important contributions to the development of

    reinforced concrete design specifications in the United States—the Joint

    (Committees on Standard Specifications for Concrete and Reinforced

    Concrete, and committees of the American Concrete Institute(1).

    The Joint Committees have consisted of delegates from the American

    Concrete Institute (ACI), American Institute of Architects (AIA),

    American Railway Engineering Association (AREA), American Society

    of Civil Engineers (ASCE), American Society for Testing Materials

    (ASTM), and the Portland Cement Association (PCA). The first, second

    and third Joint Committees were organized in 1904, 1919 and 1930, and

    submitted final reports in 1916, 1924 and 1940 respectively. These reports,

    which were milestones on the road of progress and had a strong effect

    on American concrete usage, were submitted to the constituent organiza-

    tions. The sections concerning reinforced concrete design were written in

    the form of a recommended practice rather than a design code, so that it

    was possible to give a broad reflection of the state of the art as represented

    by the best practice of the day.

    The first committee on reinforced concrete of the ACI, then the

    National Association of Cement Users (NACU), was the Committee on

    Laws and Ordinances. The first report of this committee appeared in 1909

    and was essentially based on what has later become known as ultimate

    strength design. The report was later revised to introduce the concepts of

    the straight-line theory, allowable stresses, and service loads; and it was

    then adopted as “ Standard Building Regulations for Reinforced Con-

    crete “ in 1910. Later a Committee on Reinforced Concrete and Building

    Laws was formed, sponsoring ‘

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    numerous cities and municipalities throughout the United States. Many

    agencies of the U.S. Government also refer to the ACJ Code, though

    minor adjustments are often made to suit their particular needs.

    In the field of bridge design and construction, specifications have been

    developed and periodically revised by the American Association of State

    Highway Officials and by the Ameriean Railway Engineering Association.

    NOTATION

    The letter symbols used are generally defined where they are first

    introduced; they are also listed below for convenient reference.

    Loads and load factors

    B = effect of basic load consisting of dead load plus volume change

    due to elastic and inelastic actions, shrinkage and temperature

    E =

    effect of earthquake forces

    Fb

    = ultimate strength for balanced condition given by equation (I 5)

    FO =

    ultimate strength of concentrically loaded column given by

    equation (12)

    FU =

    ultimate strength of eccentrically loaded member

    Fu’ =

    maximum axial load on long member given by equation (21)

    K = load factor equal to 2.0 for columns and members subject to

    combined bending and axial load, and equal to 1”8 for beams

    and girders subject to bending

    L = effect of live load plus impact

    MU = ultimate resisting moment

    U =

    ultimate strength capacity of section

    W =

    effect of wind load

    Cross-sectional properties

    AC =

    A, ==

    A,C =

    A,f =

    A,, =

    b=

    b, =

    ;=

    D, =

    d, =

    gross area of concrete section

    total area of IIongitudinal reinforcement

    area of compressive reinfcwcement

    steel area to develop compressive strength of overhanging flange

    in T beams, defined by equation (11)

    area of tensile reinforcement

    width of a rectangular section, or overall width of flange in

    T beams

    width of web in T beams

    n.dl = depth to neutral axis

    total diameter of circular section

    diameter of circle circumscribing the longitudinal reinforcement

    in circular section

    effective depth to centroid of tensile reinforcement

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    d, =

    effective depth to centroid of compressive reinforcement

    e= eccentricity of axial load measured from the centroid of tensile

    reinforcement

    e’ = eccentricity of axial load measured from plastic centroid of

    section

    e~’ = eccentricity of loacl

    Fb

    measured from plastic centroid of section

    L =

    unsupported Iengtlh of an axially loaded member

    nudl =

    depth to neutral axis at ultimate strength

    A,,

    r

    =

    ratio of tensile reinforcement .= —

    bdl

    rb =-

    ratio of balanced tensile reinforcement defined by equation (6)

    A

    r’ =

    ratio of compressive reinforcement = ~

    bd,

    A,,

    rt =

    ratio of total reinforcement = —

    AC

      t

    rW =—

    b’d,

    t

    = flange thickness in T section, or total depth of

    section

    Properties of’materials

    ECU =

    =W =

    f=

    U

    f

    Y ‘“

    k, =

    k, =

    mu =

    mu’ =

    maximum strain in concrete at ultimate strength

    0“003)

    strain in tensile reinforcement at ultimate strength

    stress in tensile reinforcement at ultimate strength

    :ctangular

    limited to

    yield point stress of reinforcement (limited to 60,000 lb/in2)

    ratio of average compressive stress to 0.85

    u.+,

    at ultimate

    strength

    ratio of depth to resultant of compressive stress and depth to

    neutral axis at ultimate strength

    0“85

    U y

    mu—l

    =

    cfy

    a—

    ucy/

    U.yl =

    compressive strength of 6

    x

    12 in. cylinders at 28 days

    5

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    Report of ASCE-ACI Joint Committee

    on Ultimate Strength Design

    Advancement in the field of structural design and analysis must of

    necessity proceed with extreme caution and deliberation. This has been

    true of the recommendations in the report of the ASCE-ACI Joint

    Committee on Ultimate Strength Design which culminates over ten years

    of continuous study of the subject. The joint committee was formed as a

    sub-committee of the ASCE Committee on Masonry and Reinforced

    Concrete under the chairmanship of the late A, J. Boase in 1944. It

    immediately commenced a comprehensive study of the adequacy of various

    ultimate strength theories and design formulae. As a result of its studies,

    it initiated extensive series of both short-time and sustained load tests on

    eccentrically loaded columns. These tests have been completed under the

    sponsorship of the Reinforced Concrete Research Council of the

    Engineering Foundation.

    In 1949 L. H. Corning was made chairman of the sub-committee. At

    this time, the sub-committee further recommended an extensive test pro-

    gramme on the shear resistance of reinforced concrete members. Extensions

    of this investigation are still in progress. In 1952 the sub-committee was

    made a joint committee o:f AC1 and ASCE and designated as Committee

    327 by ACI.

    Hand in hand with the :studies made on ultimate strength formulae, the

    joint committee has investigated the question of overload factors in terms

    of the practice prevailing in countries where design by ultimate strength is

    in practical use, and of the factors of safety implied in conventional

    straight-line design methods.

    During the annual convention of ACI in 1952, the joint committee

    sponsored a symposium on ultimate strength design(3). This provided an

    opportunity for public discussion of such topics as reasons for changing

    design method, fundamental concepts of ultimate strength design, review

    of research, practical design, and overload factors.

    In 1955 the committee completed its assignment “ to evaluate and

    correlate theories and data bearing on ultimate strength design procedures

    with a view to establishing them as accepted practice “. A final report was

    submitted to ASCE and AC1 4’5). It is the principal purpose of this paper

    to discuss the contents of that report, and to present the author’s opinions

    and interpretations regard ing the report.

    NATURE OF THE REPO RT

    The joint committee report presents recommendations and formulae for

    ultimate strength design (of reinforced. concrete structures together with

    basic supporting and explanatory data. The report is confined to design

    of cross-sections; it does not deal with evaluation of external moments

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    and forces. The committee recognized limit design as important but did

    not recommend practical use thereof at the present time.

    The report is based on the assumption, therefore, that structural analysis

    will be carried out by the theory of elastic displacements. On the basis of

    this assumption stresses will remain within the elastic limits under service

    loads when proper load factors are used. For statically determinate mem-

    bers, the ultimate capacity equals the computed capacity. For indeter-

    minate structures, it is important to note that the maximum moments at

    various sections are usually due to different load arrangements. Because

    of moment redistribution at high loads, therefore, the maximum load

    capacity of the indetermini~te structure may considerably exceed that

    indicated by the capacity at a single section. Accordingly, a combination

    of ultimate strength design of sections and elastic structural analysis may

    be conservative in some cases, but it is not at all unreasonable.

    The joint committee report as published by ASCE(4) consists of a brief

    section on historical background, and the essence of the report appears

    under the heading “ Recommendations for design “ Three appendixes

    deal with substantiating test data, design aids, and derivation of formulae.

    The report ends with a selected bibliography. The AC I publication (sJ

    does not contain the appendixes concerning test data and derivation of

    formulae.

    LOAD FACTORS

    Consideration was given by the joint committee to the circumstance

    that ultimate strength design may be carried out in two ways. Moments

    and forces acting at various sections may be evaluated for service loads,

    Sections may then be designed by “ deducted “ or “ allowable “ ultimate

    strength equations, in which chosen safety factors are incorporated.

    Another alternative is LOmultiply the, service loads by chosen load factors

    before the cross-section forces are evaluated. The design of sections then

    takes place by equations expressing actual ultimate strengths.

    The joint committee chose to follow the second alternative, principally

    because ultimate strength equations are essentially factual in nature, while

    the choice of load factors to a considerable extent is a matter of engineering

    judgment. By keeping load factors and strength equations separated, the

    report should be conveniently useful even to specification-writing bodies

    that find it necessary for special applications to change the numerical

    values of the load factors recommended by the joint committee. Further-

    more, it is believed to be wise for a designer clearly and unmistakably to

    keep his load factors in view.

    Two criteria were consic[ered as a basis for selecting load factors.

    Members should be proport.ioned so that: (l) they should be capable of

    carrying service loads with ,ample safety against an increase in live load

    beyond that assumed in design and against other uncertainties; (2) the

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    strains under service loacls should not be so large as to cause excessive

    cracking. The committee found that these criteria are satisfied by the

    following formulae.

    (1) For structures in the design of which effects of wind and earthquake

    forces can properly be neglected:

    U=I”2B+2.4L . . . . . . . . . . . . . . . . . . . . . . . ...(1)

    and

    U= K(B -I- L), . . . . . . . . . . . . . . . . . . . . . . . . ...(2)

    in which

    U= ultimate strength capacity of section

    B ==effect of basic loald consisting of dead load plus volume changes

    dueto elastic and inelastic actions, shrinkage, and temperature

    L = effect ofliveload plus impact

    K = load factor equal to 2“0 for columns and members subject to

    combined bending and axial load, and equal to 1”8 for beams and

    girders subject to bending

    (2) For those structures in which wind loading should be considered:

    U~l”2B+ 2”4L+O”6W . . . . . . . . . . . . . . . . ..(la)

    U=1”2B+ 0.6L+2”4W . . . . . . . . . . . . .

    . . . ..(lb)

    and

     

    )

    =K B+ I +; . . . . . . . . . . . . . . . . . . . .

      )

    ==K B+:C+W . . . . . . . . . . . . . . . . . . . .

    (2a)

    (2b)

    (3) Forstructures inthe design of which earthquake Ioading must be

    considered, substitute for the effect of wind load, W, the effect of earth-

    quake forces, E.

    GENERAL REQUIREMENTS

    The joint committee report does not deal with the many detailed require-

    ments involved in reinforced concrete design and construction, such as

    spacing and cover of reinforcement, and special considerations regarding

    the various typical bui[ding elements. A reference is therefore made to

    the ACI Building Code in all matters not otherwise provided for in the

    committee report.

    It is required” that bending moments should be taken into account in

    calculating the ultimate strength of compression members. Analysis of

    indeterminate structures should be carried out by the theory of elastic

    displacements, though approximate coefficients such as those recom-

    mended in the ACI code are acceptable for the usual types of buildings

    In structures such as arches, the effect of shortening of the arch axis,

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    temperature, shrinkage, and secondary moments due to deflexion should

    be considered.

    The committee report also calls attention to the need for checking

    deflexion of members including effects of creep, especially for high

    percentages of reinforcement.

    In considering the recommended ultimate strength equations, it is im-

    portant to note that the committee assumed that only controlled concrete

    will be used in construction of structures designed by ultimate strength.

    The quality of concrete should then be such that not more than one test

    in ten has an average compressive strength less than the strength assumed

    in design, and the average of any three consecutive tests should not be

    less than the assumed design strength. In this manner, the design concrete

    strength is not an average strength; with a reasonable probability it is a

    minimum strength. Similarly, through the general reference to the AC1

    code, the joint committee assumed that design values for the yield point

    of reinforcing steel are minimum values. Accordingly, the ultimate strength

    design equations should express an average and not a minimum relation-

    ship between ultimate strengths of the various reinforced concrete members

    as observed in tests and the cclrresponding compressive strengths.

    BASIC ASSUMPTIONS FOR IJLTIMATE STRENGTH

    After a thorough study of many ultimate strength theories presented in

    Europe as well as in America, the committee recommended that the

    calculation of ultimate strengtlh be based on the following assumptions.

    (1) As ultimate strength is approached, stresses and strains are not

    proportional, and the distribution of compressive stress in sections subject

    to bending is non-linear. The diagram c~f compressive concrete stress

    distribution may be assumed a rectangle, trapezoid, parabola, or any other

    shape which results in ultimate strength in reasonable agreement with

    comprehensive tests. In addition to this broad assumption, the joint

    committee recommended a specific set of limiting equations for various

    typical design cases as discussed in the following pages. These limiting

    equations are in good agreement with comprehensive tests of reinforced

    concrete, and calculated ultimate strengths based on a chosen stress

    distribution should therefore not exceed these given limits.

    (2) Plane sections normal to the axis remain plane after bending. When

    deformed reinforcing bars are used,

    this assumption has been verified

    even for high loads by numerous tests to failure of eccentrically loaded

    columns as well as of beams subject to bending only.

    (3) Tensile strength in concrete is neglected in sections subject to bend-

    ing. When normal percentages of reinforcement are used, this assumption

    leads to results in good agreement with tests. For very small percentages

    of reinforcement it is on the conservative side.

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     4) Maximum concrete strain in ffexure is limited to 0.003. This is a safe

    value; most strains observed in tests of reinforced concrete members fall

    between 0“003 and 0“0015‘G).

    (5) Maximum fibre stress is assumed not to exceed 85~0 of the com-

    pressive strength of 6

    x 12

    in, cylinders, A maximum stress near 100~0 of

    the cylinder strength has been found in tests of horizontally cast mem-

    bers’7’. In vertically cast members such as columns, however, due to water

    gain resulting in a lower strength near the top, and due to effects of size

    and shape, a maximum stress of 8.5’~ of the cylinder strength has been

    observed ‘8’9’.Since some effect of size and shape probably also is present

    in large beams, and since the concrete near the top of beams as well as

    columns may be somewhat weaker than control cylinders, it seems

    reasonable in all cases to use an 8.50/0 stress.

    (6) Stress in tensile and compressive reinforcement at ultimate strength

    is assumed not to exceed the yield point of the steel used or 60,000 lb/in2,

    whichever is smaller. The purpose of the 60,000 lb/in2 limit is, of course,

    to avoid excessive cracking under service loads. This limit is conservative,

    considering the high effectiveness of the bar deformations that are now

    in use throughout our country. It is also possible, to some extent, to

    control cracking by other variables than steel stress.

    RECTANGULAR BEAh4S

    To establish limiting equations for ultimate strength in the various

    cases, the joint committee chose a theoretical approach originated by

    F. Sttissi of Switzerland in 1932 and based on the general properties of

    the stress distribution shown in Figure 1. The properties of the stress

    l-- b l

    l

    h:

    J

    c

    —.

    As,

     

    Figure 1: Flexwd analysis.

    block are given by the stress factor O“85kl (German: Volligkeitsgrad) and

    the centroid factor

    k2

    (German: Schwerpunktsbeiwert). Equilibrium of

    forces and moments then gives:

    -4s,j_,U=0.85 klu@c.. . . . . . . . . . . . . . . . ..(1)

    ,MU= 0.85kluCY@c(dl—I@ . . . . . . . . . . . . . . . . . .(2)

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    When tension controls ultimate strength, the ultimate steel stress f,U

    equals the yield point Y;, and the ultimate resisting moment obtained by

    solving equations (1) and (2,) is given by:

    /

    in which

    AS, =

    d, =

    O“85k1 =

    k, =

    ucy/ =

    r

    b=

     

    k,

    rfy

    )

    MU= A,lfydl I—-—— . . . . . . . . . . . . . . .

    0.85k1 UCY,

    }

    (3)

    area of tensile reinforcement

    yield point stress of reinforcement (limited to 60,000 lb/in2)

    effective depth

     t

    centroid of tensile reinforcement

    stress factor, ratio of average compressive stress to uCYl

    centroid factor,, ratio of depth to resultant of compressive

    stress and depth to neutral axis

    compressive strength of 6x 12 in. cylinders at 28 days

    A,,,

    ratio of reinforcement = —–

    bdl

    width of beam

    The quantities kl and k2 are fundamental properties of concrete that

    have been determined by direct tests of plain concrete specimens(T).

    Equation (3) is then a fully rational equation developed by the equations

    of equilibrium from measured properties of the materials steel and

    concrete.

    Equation (3) may also be developed on a more empirical basis by study-

    ing the results of reinforced concrete beam tests. The author recently

    determined the coefficient –—

    ~~k from published data on 364 beam tests

    1

    by the statistical method c)f least squares, and the value of 0“593 was

    0.5

    found. A value of— =

    0.59 was suggested by C. S. Whitney over ten

    0“85

    years ago[lO), and this value is also in good agreement with the direct

    tests of plain concrete(7’.

    It is entirely reasonable, therefore, that the joint committee recom-

    mended that the computed ultimate moment of beams should not exceed

    that given by

      )

    W=A,,,fYdl 1-–0.59:/ . . . . . . . . . . . . . ...(4)

    CY

    which can be re-stated as

    Mu

    —=q(l-– 0.59q) . . . . . . . . . . . . . .

    . . ..(4a)

    z, .,,

    rfy

    in which q ==—.

     Y

    When compression controls ultimate strength, the steel stress at failure

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    may be determined by considering linear distribution of strain (Figure 1):

    dl — c

    E

     U

    = Ecu-— . . . . . . . . . . . . . . . . . . . . . .(5)

    c

    Combining equations (1) and (5) and seeking the balanced reinforcement

    ratio for which

    f,. = fY, we

    obtain

    Ecu

    U@

    ‘b= ”85k’k

    h“”””””””’”””’”’”””

    j-- +

    Ecu

    ~s

     6)

    The maximum ratio of reinforcement in equation (4) should be some-

    what less than the balanced ratio given by equation

    (6).

    Choosing a

    limiting value of

    r

    equal to about 90’70 of

    r~,

    the joint committee recom-

    mended that

    r

    should not exceed

    r=o.40@’ . . . . . . . . . . . . . . . . . . . . . ...(7)

    f

    in which the coefficient 0.40 is to be reduced at the rate of 0“025 per

    1,000 lb/in2 concrete strength in excess of 5,000 lb/inz. Such reduction

    for high concrete strength is desirable on the basis of several experimental

    studies that indicate a decrease of the stress factor,

    0.85k,,

    with increasing

    concrete strength (7,11’.

    When the ratio of reinforcement exceeds that given by equation (7),

    compression reinforcement must be provided. For this case, the joint

    committee recommended that the resisting ultimate moment should not

    exceed

    MU = (AS*— AJj;dl 1— 0.59(r -– r’)~

    1

    + f J d,d, ) 8)

    Ury(

    in which (r — r’) should not exceed the value given by equation (7), and

    A C=

    area of compressive reinforcement

    A

    r’ =

    ratio of compressive reinforcement = ~

    bd,

    d2 =

    effective depth to centroid of compressive reinforcement

    For beams with the usual amounts of reinforcement dictated by economy

    and spacing of reinforcing bars,

    r

    is 0.15 to 0.25 times 4[, and there is

    f,

    little difference between designs resulting from ultimate strength and

    straight-line procedures. The major changes suggested by the committee

    therefore concern a more efficient use of reinforcement with yield points

    over 40,000 lb/in*. In present American design codes based on straight-

    line theory a ceiling allowable stress of 20,000 lb/inz is used for such

    reinforcement, while the ultimate strength design method as outlined may

    lead to the equivalent of a.n ailowable stress of 60,000/ 1.8 =. 33,300 lb/in2.

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    As a second change it is made possible, when economically and practically

    feasible, to utilize more fully the strength of the concrete compression

    zone.

    T SECTIONS

    If the neutral axis falls within the flange of a T beam, the equations for

    rectangular beams are applicable with r cc~mputed as for a beam with a

    width equal to the overall flange width. The depth to the neutral axis, c,

    may be estimated by solving equation (1):

    1 r~d

    c=n@~l=—’—

    0“85k1uCYl 1“””””’””””””””””’”

    .

    .(9)

    In this case, the joint committee recommended a conservative value of

    c = l“30rfy4.

    Ucyl

    When c is greater than the depth of the flange, the tensile reinforcement,

    A,,, may be considered subdivided into one part, A,f, that will develop

    the compressive strength of the overhanging portion of the fldnge and

    another part,

    (A,f — A,f),

    that will develop the compressive strength of a

    a portion of the web. Assuming a uniform stress of 0“85uCYZn the flange,

    the joint committee recommended:

    [

    1

    u=A, ,At f ) j j i ,— 0.59(r~ — rf) + A,f~(dl — ~“5t). .(10)

    CY

    in which A,f is the steel area necessary to develop the compressive strength

    of the overhanging flange:

    A,~=O”85@- lY)~l . . . . . . . . . . .

    . . . . . ..(11)

    h

    and

     

    flange thickness

    b = overall width of flange

    b’ = width of web

    r =2

    :dl

    AS,

    ‘w = b’dl

    A,f

    rf=—

    b’dl

    In equation (10) the value of (rW— r~) should not exceed that given by

    equation (7).

    13

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    CONCENTRICALLY LOADED SHORT COLUMNS

    The joint committee recognized that the strength of concentrically

    loaded short columns is given by

    Fo=0.85uC,vlAC +A,~ . . . . . . . . . . . . . . . . . . ..(12)

    in which

    AC = gross area of concrete section

    A, = total area oflcmgitudinal reinforcement

    It wasrecommended, however, that all members subject to axial loads

    should be designed for at least a minimum eccentricity. For spirally rein-

    forced columns the cc)mmittee gave a minimum eccerrtricity measured

    from the centroidal axis equaI to 0.05 times the depth of the column

    section; for tied columns O.10 times the depth was recommended.

    This recommendation involves a change from present practice which

    limits the allowable load for a tied column to 80 of that for a spirally

    reinforced column. This change seems reasonable since in practice very

    few columns are trul~y concentrically loaded, and recent tests(g) have

    indicated that for columns with even a small eccentricity of load, no

    second maximum Ioad is developed due to spiral action.

    ECCENTRIC LOAD, F~ECTANGULAR SECTION

    The uItimate strength of members subject to combined bending and

    axial load may be computed from tlhe usual two equations of equilibrium,

    b

    C

    ——

    Figure 2:

    Eccentric load analysis.

    which, when the neutral axis is within the section, may be expressed as

    follows (Figure 2):

    FU = ().85klUcY~hnudl+ A.C~Y— ,4.,~,u. . . . . . . . . . . . . . (13)

    Fue = 0085kluCY@Ud12(l— k2n.) + A,~L(dI -– dz). . . . . . . (14)

    in which

    FU =

    ultimate eccentric axial load

    14

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    e

    = eccentricity of the axial load measured from the centroid of

    tensile reinforcement

    Au = stress in tensile reinforcement which equals ~Y when tension

    controls ultimate strength, but is smaller than ~Y when com-

    pression controls

    nudl = c = depth to neutral axis at ultimate strength

    In the above equations, the joint committee recommended that k,

    should not be taken as less than

    ~kl,

    and hl should not be greater than

    0“85 for UCY1 5,000 lb/in2. The coefficient ().85 should be reduced at the

    rate of 0“05 per 1,000 lblinz concrete strength in excess of 5,000 lb/in2.

    By solving equations (5) and (,13) forj~U ==f, and ECU= 0.003, it is found

    that the ultimate load for the balanced condition is given by

     

    0.003E,

    F~ = 0-85k1 ——

    0“O03E, + f, )

    UQ@dl + (Asc — z4Jfy . . . . . .

    (15)

    When FU is less than the value of Fb given by equation (15), ultimate

    strength is controlled by tensicm and .fiU= fY. Taking into account the

    concrete area displaced by the compression reinforcement and solving

    equations (13) and (14) for the ultimate strength, we then obtain:

    1

     ) \

    FU = 0.85uCYlbd1

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    A linear relationship between axial load and moment may be assumed

    for values of

    FU

    between

    Fb

    as given by equation (15) and the concentric

    ultimate load Fo given by equation (12). For this range the ultimate

    strength may therefore be computed by

    FO

    FU=—

    ()

    . . . . . . . . . . . . . . . . . . .

    (17)

    1+ ;—15

    eb’

    in which

    e’ == eccentricity measured from plastic centroid of section

    e~’ = eccentricity of load Fb measured from plastic centroid of section

    as computed bly solution of equations (14) and (15).

    The plastic centroid of a section is computed with a “ modular ratio “

    m“ = ~

    For symmetrical reinforcement, the plastic centroid coin-

    0.85uCY,“

    tides with the geometric centroid.

    The joint committee also recognized the equation developed by

    C. S. Whitneytl”j for ultimate strength when compression controls:

    A,Cu + - btu,,,

    Fu= —

    . ... . . . . . . . . . . .

    (18)

    e’

    —“

    ;+1”18

    d, — d,

    1

    in which

      total depth of section.

    Though we] 1 substantiated by test data, the methods presented above

    for the ~esign of eccentrically loaded rectangular sections involve a major

    change from present American practice. Even though the principle of the

    addition law as expressed by equation (12) is recognized in present design

    codes for small eccentricities, the safety factor with respect to ultimate

    strength may vary frc~m near one to over four, depending on the com-

    bination of variables involved. By the proposed ultimate strength design

    procedures, a much more uniform safety factor will be obtained. It should

    also be noted that l.he mathematical equations involved are greatly

    simplified as compared to a modified straight-line theory.

    ECCENTRIC LOAD, CIRCULAR SECTION

    The ultimate strength of members of circular cross-section subject to

    combined bending and -axial load may be computed on the basis of the

    equations of equilibrium taking inelastic deformations into account. The

    joint committee also recommended use of a modification of the partially

    rational and partially empirical formul~ developed by C. S. Whitney (9.10).

    16

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    When tension controls:

    FU= 0“85uCYlD~

    {/(

    0.85e’

    )

    ——0.38 2 + ‘%

    D

    -(

    )

    ~-O.38 } . . . . . . . . . . . . ..(19)

    When compression controls:

    4fy _

    Fu=—

    ACuCYl

    . . . . . . . . . .

    (20)

    :+ 11

    9“6De’

    (O%D + 0“67D )2

    + 1.18

    s

    in which

    D =

    diameter of circular column

    D, =

    diameter of circle circumscribing longitudinal reinforcement

    A,

    rt=—

    AC

    LONG MEMBERS

    For cases when the unsupported length., L, of an axially loaded member

    is greater than fifteen times its least lateral dimension, t, the joint com-

    mittee recommended that the maximum axial load,

    FM’,

    should be deter-

    mined by one of the following two methcjds.

    The effect of slenderness on ultimate strength maybe taken into account

    by stability determination with an apparent reduced modulus of elasticity

    used for sustained loads. A numerical procedure such as that recommended

    in the report of ACI Committee 312 on Plain and Reinforced Concrete

    Archestlzj may be used.

    The maximum axial load may also be determined by

      )

    U’=ZFO 1“6— O.04~ . . . . . . . . . . . . . . . .

    . .(21)

    t

    in which F. is the concentric load capacity of the section with L/ t

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    Practical applications

    After one becomes farniiiar with ultimate strength theory for reinforced

    concrete, the design equations involved are considerably simpler to use

    than those resulting from the straight-line theory, Further simplification

    of routine design calculations is nevertheless desirable. The joint com-

    mittee report’4 ) contains several charts intended to expedite the propor-

    tioning of sections by ultimate strength theory. Development of further

    design aids is in progress.

    THE AC I BUILDING CC)DE

    The joint committee report is an engineering report; it is not a building

    code, it is not a standard specification. To gain widespread practical

    application, therefore, ultimate strength design must be incorporated into

    design and building codes,. Ultimate strength design in America has now,

    in the opinion of many of us, been developed so far that extensive practical

    experience is necessary to continue progress.

    A proposed revision of the ACI Building Code was reported by ACI

    Committee 318 in December 1955(Z). This proposed revision incorporates

    the ultimate strength method of design as an alternative to tlhe straight-line

    theory, and an abstract of the joint committee report on ultimate strength

    design is given in an appendix. This proposed revision was unanimously

    adopted by the 1956 convention of the ACI.

    In this manner, after extensive scientific researches and a decade of

    thorough committee work, the ultimate strength design method has been

    placed before the engineering profession. The future of ultimate strength

    design in American practice is, therefore, now largely in the hands of

    our engineers and architects practicing the science and art of reinforced

    concrete design and construction.

    1.

    2.

    3,

    4.

    5.

    REFERENCES

    KEREKES, F. and

    REI I

    H. B. Jr. Fifty years of development in building code

    requirements for rei ttfoneed concrete. Journal oj”the American Concrete Inst itute.

    Vol. 25, No. 6. February 1954.pp. 441-470.

    Proposed revision of building code requirements for reinforced concrete (ACI

    318-51).

    Journal o f the American Concrete Institute.

    Vol.

    27, No. 4.

    December

    1955. pp. 401-445.

    CORNING, L, H., ANDERSON, B. G,, HOGNESTAD, Ii, SIESS, C. P.,

    REESE, R. C. and LIN, T. Y. Symposium on ultimate strength design.

    Journal

    of the Ainerlcan Concrete Institute. Voll. 23, No. 10. June 1952. pp. 797–900.

    Report of ASCE-ACI J,Dint Committee on ultimate strength design. Proceedings

    of the American Society of Civil Engineers.

    Vol. 81, October 1955. Paper 809.

    pp. 68.

    ACI-ASCE COMMITTEE 327. Ultimate strength design.

    Journal of the American

    Concrete Institute. Vol. 27, No. 5. January 1956. pp. 505-524.

    1 3

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    6. Discussion of a paper by E. Hognestad: Inelast ic behaviour in tests of eccentrically

    loaded short reinforced concrete columns. Journal of the American Concrete

    Instiiure.

    Vol.

    25, No. 4.

    Dec[:mber 1953. Fig. G. p. 140/13.

    7. HOGNESTAD, E., HANSC)N, N. W. and McHENRY, D. Concrete stress

    distribution in ultimate strength design. Journal o~the American Concrete Institute.

    Part 1. Vol.

    27, No. 4.

    December 1955. pp. 455-479.

    8. RICHART, F. E. and BROWN, R. L. An investigation of reinforced concrete

    columns. University of Illinois Engineering Experiment Station. June 1934.

    Bulletin No. 267. pp. 91.

    9. HOGNESTAD, E. A study Of combined bending and axial loud in reinforced

    concrete members. University of Illinois Engineering Experiment Station.

    November 1951. Bulletin No. 399. pp. 128.

    10. WHITNEY, C. S. Plastic theory in reinforced concrete design. Transactions of

    the American Society oj Civil Engineers. Vol. 107. 1942. pp. 25 1–282 . Discussion

    pp. 282-326.

    11. RUSCH, H. Versuche zw Festigkeit der Biegedruckzone. Deutscher Ausschuss

    fur Stahlbeton. No. 120.1955. pp. 94.

    12. Report of ACI Committee 31,2: Plain and reinforced concrete arches. Journal o f

    the American Concrete Institute. Vol. 22,No. 9.May 1951. pp. 681-.69I.Discussion

    Vol. 23, No. 4. December 1951. pp. 692/1-692/11.

    19

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    D8

    —“Resurfacing and patching Concrete Pavement with Bonded Con-

    crete,”

    by EARL J. FEL r.

    lteprintedfrom Proceedings OJthe H{phuau Research Boar d 5  1956 ,

    D9

    —“Review of Data on Effect of Speed in Mechanical Testing of Con.

    crete,”

    by

    DOUGLAS MCHENRY and J. J. SIIIDELER.

    Reprinted from Speeiat Tectmical PubUcation No, 185, published by Ameri-

    can Society for Testing Materials 1S5S).

    DIO-’’Laboratory Investigation of Rigid Frame Failure,” by R. C.

    ELST-

    NER and E. HOGNESTAO.

    Reprinted from Jrournulof the Amertcan Concrete

    Institute

     anuary, 1957);

    proceedings, 53, 637 1957).

    D12-’’Ultimate Strength of IReinforced Concrete in American Design Prac-

    tice,” by EMND HOCNESTAD.

    Reprinted from

    Proceedings of a S mpos@n on the Strength of Concrete

    Structures, Lond,m, May, 1956.