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CE 809 - Structural Dynamics Lecture 5: Response of SDF Systems to Impulse Loading Semester Fall 2020 Dr. Fawad A. Najam Department of Structural Engineering NUST Institute of Civil Engineering (NICE) National University of Sciences and Technology (NUST) H-12 Islamabad, Pakistan Cell: 92-334-5192533, Email: [email protected] Prof. Dr. Pennung Warnitchai Head, Department of Civil and Infrastructure Engineering School of Engineering and Technology (SET) Asian Institute of Technology (AIT) Bangkok, Thailand

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Page 1: PMCE Structural Dynamics - Home - StructuresPro

CE 809 - Structural Dynamics

Lecture 5: Response of SDF Systems to Impulse Loading

Semester – Fall 2020

Dr. Fawad A. Najam

Department of Structural Engineering

NUST Institute of Civil Engineering (NICE)

National University of Sciences and Technology (NUST)

H-12 Islamabad, Pakistan

Cell: 92-334-5192533, Email: [email protected]

Prof. Dr. Pennung Warnitchai

Head, Department of Civil and Infrastructure Engineering

School of Engineering and Technology (SET)

Asian Institute of Technology (AIT)

Bangkok, Thailand

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Impulse Loading

• Impulsive forces, shock loads, short duration loads.

• Impact, blast wave, explosion

• Sudden stop/break of trucks & automobiles & travelling cranes

The study of impulse response is also important for the analysis of response to arbitrary

loadings.

Page 3: PMCE Structural Dynamics - Home - StructuresPro

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Response to Impulse Loading

Response

𝑝 : Step Impulse

𝑝𝑜

𝑇

𝑡No Load

Decayed

Oscillation

∆𝑡

Phase I: Loading Phase

Phase II: Free Vibration Phase

(𝑡)

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Response to Impulse Loading

Impulse Force Magnitude = 𝑝𝑜, start at 𝑡 = 0, Duration = Δ𝑡, where Δ𝑡/𝑇 << 1

Initial at-rest: 𝑢 = 0, 𝑢 = 0Structure (0) (0)

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Response to Impulse Loading

Phase 1:

The particular solution to a step

loading is simply a static deflection:

𝑝𝑜

𝑡∆𝑡

𝑝 𝑡

𝑡 ……….. (1)𝑢𝑝 =𝑝𝑜𝑘

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Response to Impulse Loading

This solution satisfies the equation of motion:

𝑢𝑝 = 0

𝑢𝑝 = 0

Substitute the above relations into the equation of

motion:

Phase 1:

0 + 0 + 𝑘𝑝0𝑘

= 𝑝0

𝑢𝑝 =𝑝𝑜𝑘

𝑡

𝑡

𝑡

𝑚 𝑢𝑝 + 𝑐 𝑢𝑝 + 𝑘 𝑢𝑝 = 𝑝0𝑡 𝑡 𝑡

Page 7: PMCE Structural Dynamics - Home - StructuresPro

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Response to Impulse Loading

A general solution:

𝑢 = 𝑢𝑝 + 𝑢ℎ

𝑢 =𝑝𝑜𝑘+ 𝑒−𝜉 𝜔 𝑡 𝐴 sin 𝜔𝐷𝑡 + 𝐵 cos 𝜔𝐷𝑡

Where

𝐴 and 𝐵 are determined such that the at-rest initial conditions are satisfied.

Phase 1:

……….. (2)

(𝑡) (𝑡) (𝑡)

𝑡

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Response to Impulse Loading

𝑢 =𝑝𝑜𝑘+ 𝐵 = 0

𝑢 = 𝜔𝐷𝐴 − 𝜉𝜔𝐵 = 0

So we obtain:

Phase 1:

𝐵 = −𝑝𝑜𝑘

𝐴 =𝜉𝜔𝐵

𝜔𝐷

……….. (3)

0

0

𝑢 =𝑝𝑜𝑘+ 𝑒−𝜉 𝜔 𝑡 −

𝜉 𝜔

𝜔𝐷

𝑝𝑜𝑘sin 𝜔𝐷𝑡 −

𝑝𝑜𝑘cos 𝜔𝐷𝑡

……….. (4)𝑡

(valid in the range 0 < 𝑡 < Δ𝑡)

Page 9: PMCE Structural Dynamics - Home - StructuresPro

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Response to Impulse Loading

Due to fact that 0 < 𝑡 < Δ𝑡 and Δ𝑡/𝑇 << 1 and 𝜉 << 1

𝑢 ≈𝑝𝑜𝑘−𝑝𝑜𝑘cos 𝜔𝑡 ≈

𝑝𝑜𝑘

1 − cos 𝜔𝑡

Phase 1:

……….. (5)

Equation (5) shows the approximate response during the loading phase.

𝑡

𝑢 =𝑝𝑜𝑘+ 𝑒−𝜉 𝜔 𝑡 −

𝜉 𝜔

𝜔𝐷

𝑝𝑜𝑘sin 𝜔𝐷𝑡 −

𝑝𝑜𝑘cos 𝜔𝐷𝑡

……….. (4)𝑡

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Response to Impulse Loading

Phase 2:

𝑡

𝑡 = ∆𝑡

𝑡 = 0Phase II

No Load: Free vibration response

depends on the initial conditions at

𝑡 = ∆𝑡

Page 11: PMCE Structural Dynamics - Home - StructuresPro

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Response to Impulse Loading

Phase 2:

𝑢 =𝑝𝑜𝑘

1 − cos 𝜔𝑡𝑡

𝑢 =𝑝𝑜𝑘

𝜔 sin 𝜔𝑡𝑡

𝑢 =𝑝𝑜𝑘

𝜔 sin 𝜔 Δ𝑡 ……….. (6)∆𝑡

𝑢 =𝑝𝑜𝑘

1 − cos 𝜔 Δ𝑡∆𝑡

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Response to Impulse Loading

Phase 2:

Employing Tylor’s expansion:

sin 𝜃 = 𝜃 −𝜃3

3!+𝜃5

5!……

cos 𝜃 = 1 −𝜃2

2!+𝜃4

4!……

For small 𝜃, by neglecting the second order term and higher terms, we get

sin 𝜃 ≈ 𝜃, cos 𝜃 ≈ 1 ……….. (7)

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Response to Impulse Loading

Phase 2:

Introducing this approximation in Equation (7) into Equation (6), we obtain

𝑢 =𝑝𝑜𝑘

1 − cos 𝜔 Δ𝑡 ≅ 0

𝑢 =𝑝𝑜𝑘

𝜔 sin 𝜔 Δ𝑡 ≅𝑝𝑜 𝜔

2 ∆𝑡

𝑘=𝑝𝑜 ∆𝑡

𝑚

Note that 𝑝𝑜 ∆𝑡 is an impulse.

Equation (8) says that impulse ≈ the change in momentum (of the mass)

The impulse introduces “momentum” into a structure but the duration of impulse is so

short that the displacement has not been developed yet.

……….. (8)

Δ𝑡

Δ𝑡

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Response to Impulse Loading

Using the Equation (8) as the initial conditions for free vibration in Phase 2,

𝑢 = 𝑒−𝜉 𝜔 (𝑡−∆𝑡) 𝑢

𝜔𝐷sin 𝜔𝐷 𝑡 − ∆𝑡

Since ∆𝑡/𝑡 << 1 , it is justified to let 𝑡 − ∆𝑡 ≈ 𝑡, that is

𝑢 ≈ 𝑒−𝜉 𝜔 𝑡𝑝𝑜 Δ𝑡

𝑚 𝜔𝐷sin(𝜔𝐷𝑡)

Equation (10) will be used when we analyze the response to arbitrary loading in the next

section.

Phase 2 (t > ∆𝒕 ):

……….. (9)

……….. (10)

𝑡∆𝑡

𝑡

Page 15: PMCE Structural Dynamics - Home - StructuresPro

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Response to Impulse Loading

𝑒−𝜉 𝜔 𝑡𝑝𝑜 Δ𝑡

𝑚 𝜔𝐷sin(𝜔𝐷𝑡)

𝑝𝑜

𝑡∆𝑡

Total Response

Page 16: PMCE Structural Dynamics - Home - StructuresPro

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