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D-A079 866 AEROSPACE MEDICAL RESEARCH LAB WRIGHT-PATTERSON AFB OH F/G V3USAF BXOENVIRONMENTAL NOISE OATA HANDBOOK. VOLUME 120. C-5A AIR--E TCU
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/4 1 2. ~~G O V T A C C ESSIO 3. R E C IP IE T A A O ) M E
11W jOERVIRONMENTAL.P0ISE..DATA ADBOOKD olm l2,Wf a series
7. AUTNOR(w)S.CNRCOGRN UBRa
'2 /0 Robert G. owell
Aerospace Medical Research Laboratory 73
Systems Command, Wright-Patterson AFB OH _______________
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IS, KEY WORDS (Continue on rever** side it necesaryi and Identify by block number) iUL)k jL3U U L
Noise BNoise EnvironmentsBioenvironmentaJ. Noise0-SA Aircraft
20. ABSTRACT (Continue on reverse aide if necesary and identify by block number)
-fr The USAF 0-SA is a global, strategic airlift aircraft poweredby four TF39-GE-1 turbofan engines. This report provides measuredand extrapolated data defining the bioacoustic environments pro-duced by this aircraft operating on a concrete runup pad for fiveengine/power configurations. Near-field data are reported forforty-five locations in a wide variety of physical and psycho-acoustic measures: overall and band sound levels, preferred speech
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interference level, perceived noise level, and limiting times fortotal daily exposure of personnel with and without standard Air- Force ear protectors. Far-field data measured at 19 locations arenormalized to standard meteorological conditions and extrapolatedfrom 75-8000 meters to derive sets of equal-value contours forthese same seven acoustic measures as functions of angle anddistance from the source. Refer to Volume 1 of this handbook,"USAF Bioenvironmenta Noi e Data Handbook, Vol 1: Organization,Content and Application", ARL-TR-75-50(1) 1975, for discussionof the objective and design of the handbook, the types of datapresented, measurement procedures, instrumentation, data pro-cessing, definitions of quantities, symbols, equations, applica-tions, limitations, etc.
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ARM.,-
PREFACE
This report was prepared by the Biodynamnic Environment Branch, Aerospace Medical Research Laboratory, under
Project/Task 723107, Technology v) Define and Access Enviroz na Quality of Noise From AF Operations andProject/Task 723106, Crew Safety in Operational Noise Environments.
The author gratefully acknowledges Mr. John Cole for his assistance in preparng this report, Aft. Haruld Hile for hisassistance in acquiring the raw data, Mr. Henry Mohlman, Mr. Keith Kettler and Mft. Fred Lampley of the Universityof Dayton for assistance in the mechanics of data processing and Mrs. Peggy Massie for assistance in typing andpreparation of the graphics.
~CESSION forIns White Section
DC Buft Setion
u?4ANNOUKED 1
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Table of Contents
Pap
IN TROD UCTION .............................................................................. 3
N EAR-FIELD N OISE .......................................................................... 4
FAR-FIELD N OISE ............................................................................ 9
List of Tablm
NEAR-FIELD NOISEI. Measurement Locations and Test Conditions ................................................... 5-62. Measured Sound Pressure Level
1/3 O ctave Band ......................................................................... 12-16O ctave B and ............................................................................ 17-21
3. M easures of Human Noise Exposure .......................................................... 22-26
FAR-FIELD NOISE4. T est C onditions ........................................................................... 275. M easured Sound Pressure Level .............................................................. 28-326. D irectivity Index .......................................................................... 43-47
List of Figures
NEAR-FIELD NOISE1. M easurem ent Locations ....................................................................
Plan and Elevation View .................................................................. 7Tire Inflation System and APU/ATM Exhaust ............................................... 8
FAR-FIELD NOISE2. M easurem ent Locations .................................................................... 103. Normalized Far-Field Noise Levels ........................................................... 33-374. Acoustic Power Level ....................................................................... 38-425. Overall Sound Pressure Level - Contours ..................................................... 48-526. C-W eighted Sound Level - Contours ......................................................... 53-577. A-W eighted Sound Level - Contours ......................................................... 58-628. Perceived Noise Level - Contours ........................................................... 63-679. Speech Interference Level - Contours .............................................. 68-72
10. Permissible Exposure Time - Contours ....................................................... 73-9411. Octave Band Sound Pressure Level - Contours ............................................... 95-139
2
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INTRODUCTION
The USAF C-5A is a global, strategic airlift aircraft powered by four TF39-GE-1 turbofan engines. The aircraft wasmanufactured by the Lockheed Aircraft Corporation and the engines by the General Electric Company.
This volume provides measured and extrapolated data defining bioacoustic environments produced by this aircraftduring ground runup operations. Such data are essential to evaluate ear protection requirements, limiting personnelexposure times, voice communication capabilities, and annoyance problems associated with ground runups of the C-5Aaircraft.
This volume is one of a series published by the Aerospace Medical Research Laboratory (AMRL) under the samereport number (AMRL-TR-75-50) as a multi-volume handbook that quantifies the noise environments produced atflight/ground crew locations and in surrounding communities by operations of Air Force aircraft and ground supportequipment. The far-field, community-type noise data in the handbook describe the noise produced during groundoperations of aircraft, ground support equipment, and other ground-based equipment or facilities.
Volume 1 of this handbook discusses the objectives and design of the handbook, types of data presented, measurementprocedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations,etc. Volume 2 provides a method and data for adjusting the handbook's far-field noise data, which are for standardmeteorological conditions (15 C temperature, 70% rel humidity, 0.760 meters Hg barometric pressure), to derivecomparable data for other meteorological conditions. Refer to Volumes I and 2 (references 1 and 2) for suchinformation because it is not repeated in other handbook volumes.
A cumulative index lists those aerospace systems contained in the handbook, and identifies the specific volumescontaining each type of environmental noise data available (i.e., inflight/flight crew and passenger noise,near-field/ground crew noise, far-field/community noise). Volume numbers are assigned sequentially as individualvolumes are published. This index is periodically updated as individual volumes are published and is available uponrequest from AMRL/BBE, Wright-Patterson AFB, OH 45433. Organizations on the distribution list for the handbookwill automatically receive a copy of each updated index.
Direct any questions concerning the technical data in this report and other handbook volumes to: AMRL/BBE,Wright-Patterson AFB, OH 45433; AUTOVON 78-53675 or 78-53664; Commercial (513) 255-3675 or 4513) 255-3664.
1. Cole, John N., USAF Bioenvironmental Noise Data Handbook, Volume 1: Organization, Content and Application, AMRL-TR-75-50(1), Aero6pace Medical Research [abwatory, Wright-Patterson Air Force Base, Ohio, 1975
2. Cole, John N., USAF Bioenvironmental Noise Data Handbook Volume 2: Procedure to Evaluate Effects of Non-standardMeteorological Conditions on Far-Field Noise, AMRL-TR-75-50 (2), AMRL, WPAFB, OH, 1975
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NEAR-FIELD NOISE
MEASUREMENTSAMRL acquired near-field noise data on the C-5A aircraft during ground runup operations of its turbofan engines. Forthese tests, the aircraft was located on concrete parking aprons at Wright-Patterson AFB, Altus AFB and EdwardsAFB with no significant reflecting surface in the vicinity except the ground plane. Table I lists the ground crewlocations and gives the engine power conditions. The ground-crew chief selected power conditions and near-fieldlocations gerally used during routine maintenance or engine runup for preflight checks.
At each near-field location a test engineer randomly moved a hand-held microphone in and around each location,probing all areas where a crew member's head would normally be located. He recorded all of the noise samples onmagnetic tape. During analysis of each sample, he determined the root-mean square sound pressure using a 4- or8-second integration time to derive a power-averaged level for each location.
Figure 1 shows the forty-five numbered near-field locations where ground crews are usually located for maintenanceand/or preflight checkout operations. Estimates of noise levels at other locations in the near-field are difficult since thenoise source is spatially distributed, i.e., not a point source. The noise levels at near-field locations can vary widelydepending upon relative distances from each noise source (intake noise, exhaust noise, panel resonances, internalengine noise through the engine wall, etc.).
Table 1 lists the numeric/alphabetic designators used on the data pages in this report to identify the measurementlocations and test conditions. For example, the designator 1/A means ground crew location 1 and test conditions A.
RESULTSThe measured data presented in Table 2 define the sound pressure levels (SPL) produced by the C-5A aircraft at theforty-five ground crew locations. This table includes the overall, 1/3 octave band, and octave band levels. From thesedata one can calculate the variety of measures given in Table 3 which are widely used to assess the effects of noise onpersonnel and their performance.
All near-field data are for the meteorological conditions at the time of test but are valid for all typical airbasemeteorology because of the short sound propagation distances involved.
4
TABLE 1
MEASUREMENT LOCATIONS AND TEST CONDITIONSFOR NEAR-FIEWD NOISE MEASUREMENTS
C-SA Airra, Ground RunupEdwards AFB, 6 September 1969, Tail M002
Wright-Pattro AFB, 27 April11970, Tal 0005Altu AFB, 14 June 1978, Tall 0690025
Ground Crew Locatn
I Eagiae#l Stan2 Engine #2 Start3 Engine #2 and 4 Start4 Scanner Area5 NLG, Wheel Well, Forward Part6 NLG, Wheel Well, Aft Part
Chock Removal, Forward MLG, Forward TiresChock Removal, Forward MLG, Aft Tres
9 Chock Removal, Aft MLG, Forward Tires10 Chock Removal, Aft MLG, Aft TiresI I Wing Walker12 Engine Trim13 APU Troubleshoot14 APU Leak Test15 Marshal/Telephone Talker16 PTU Leak Test17 SPR Refueling Receptacles18 Hydraulic Leak Test, Forward MLG Pod, Forward End19 Hydraulic Leak Test, Forward MLG Pod, Aft End20 Hydraulic Leak Test, Aft MLG Pod, Forward End21 Hydraulic Leak Teat. Aft MLG Pod, Aii End22 Ladder23 Engine Observation24 Hydraulic Leak Check25 APU/ATM Noise At 20 Ft. Radius, 10026 APU/ATM Noise At 20 Ft. Radius, 30027 APU/ATM Noise At 20 Ft. Radius, 60028 APU/ATM Noise At 20 Ft. Radius, 90029 APU/ATM Noise At 20 Ft. Radius, 120030 APU/ATM Noise At20 Ft. Radius, 150031 Right Aft MLG, Left Aft Tire32 Right Aft MLG, Between Aft Tires33 Right At MLG, Right Aft Tire34 Right Aft MLG, Left Forward Tire35 Right Aft MEL Right Forward Tire36 Right Aft MLG, - 10 Ft. To Right37 Right Aft MLG, Unoer TIS Exhaust38 Right Aft MLG. 3-5 Ft. Forward TIS Exhaust39 Right Forward MLG, Left Aft Tire40 Right Forward MLG, Right Aft Tire41 Right Forward M ]L, eft Forward Tire42 Right Forward MW, Right Forward Tire43 Left Forward MLG, Right Aft Tire44 Left Aft MLG, Right Forward Tire45 Left Aft MLG, Right Aft Tire
Aircraft Engine end Power Unit Operations
A Engine #1 Idle, APU and ATMONB Engine #1 - 2 Idle, APU and ATMONC Engine #1, 2, and 3 Idle, APU and ATM ON
A
D Ad Enigine Idle, APU and ATM ONE All Engines 2.0 EPR, AnU and ATm ONFG Engine #3 Idle, APU 4M ATM ONH Engine 03 i:.d EPR, APU and ATM ON
Engine #3 4.26 EPR, ApU and ATM ONAPU On,AllEEngiesOFFK1 PTU ON (Flaps Operated To Load PTU), Engines OFFK ATM and APU ON, All Engines OFFL Tire nflton SyteM ON, AUl Engines OFF
ABBREVIATIONS
ATM - Awiar rieMoo T PoerTafer UnitATM - Aiiry Powbier Ut MWG - Main Landing GearEPR - Engine Presaure Ratio TU - PTir nfiontNWG - Nose Landing Gear TSR -rSuge Poi temn
Meteorology SR-Snl on euln
Akus AFB, Locaion I5and 22 through 30Temperature 27.8 C l*ta $nAB, L"dton 31 through 45Bar Pressure 0.727 M Hg Temperature 21 CKBe Hmdity d~MS~ 5T4% Wind-peed 0.6Mli ( KReWindit 4 Spe 3.R/e 7KSel Humidity 73%a- Direction 160 Deg Wn pe . /e 7KS
Temperature 27 CBar Pressure 0.699 M HgRel Humidity 33 %
MLGHEE WELLSWLL
F~gure . Near-Field Measurent Locations, Plan and Elevation View
7
0 00LET F RIGHT FWD MLG
I LEFT FWD MLG
: ~ I R Ir= NFLATONOMPRESSION EXHAUST/
i3
x 1,4
LEF RIGHT AFT MLG
APU/ATM EXHAUST
30 ,\, 150*
90\
figure 1. Near-Field Measurement Locations Around Tire@ and APU/ATM Exhaust
8
FAR-FIELD NOISE
MEASUREMENTSAMRL acquired far-field data during a one hour test period, thus keeping similar mc. 3rological conditionsthroughout the test. Figure 2 shows the ground runup pad, ground cover (short grass), aircraft orientation and the 19microphone measurement sites on a semicircle. The center of the 100 meter radius semicircle used in surveying theTF39-GE-1 engines was on the ground directly below the intersection of the aircraft's centerline and the plane passingthrough the inboard engines' exhaust-nozzle exits. The ground runup area did not have a blast deflector; therefore, theengines' exhausts were in a "free-flow" condition.
Table 4 provides cockpit readouts of some engine characteristics (% RPM, fuel flow, etc.) for each power setting usedin the far-field tests. Also listed in this table are the surface meteorological conditions during data acquisition.
All microphone measurement sites are in the acoustic far-field of the source where the sound wavefronts sphericallydiverge and the noise source may be regarded as a point source.
A portable microphone/tape-recorder system was used to sequentially record the noise at each far-field location. Themicrophone was attached to a hand-held pole, pointed at the source (00 angle of incidence) and vertically scanned from0.5 to 3 meters for a period of 5-10 seconds during data acquisition at each microphone location. These samples werethen time-integrated to derive a root-mean-square sound pressure level. Vertical scanning and time-integrating togetherreduce anomalies frequently present in data acquired by a fixed height microphone.
RESULTSTable 5 lists the overall and 1/3 octave band SPL measured at the far-field locations under meteorological conditions atthe time of the test. Data in all other figures and tables are based on these levels. These data were normalized to 100meters distance and standard meteorological conditions (15 C temperature, 70% relative humidity, 0.760 meter Hgbarometric pressure) and used to derive the graphic data in Figure 3 which provides a compact summary of the far-fieldnoise characteristics of the C-5A aircraft in a standard format.
Figure 4 and Table 6 present two basic acoustic measures, the acoustic power level and the directivity index,respectively. The acoustic power level describes the power radiated by the source as a function of frequency. Thedirectivity index is a standard acoustical engineering measure which describes the geometric way in which the sourceradiates this power as a function of both frequency and angle from source. These basic source measures are primarily ofinterest for acoustical engineers and noise generation/control specialists.
9
L GRASSWASPHALT
Figure 2. Far-Field Measurement Locations at Altus AFB OK
10
Estimates of noise characteristics for intermediate power settings (e.g., 88% engine) and/or different number ofengines operating (e.g., single engine) can be determined as explained in Volume I of this handbook.
Figures 5 through 11 are sets of equal noise contours describing seven different measures of noise as a function of angleand distance from the source for standard day meteorology. They are respectively, overall sound pressure level,C-weighted sound level, A-weighted sound level, perceived noise level, speech interference level, permissible exposuretimes for personnel and octave band sound pressure levels.
- INo data are presented at the 180 degree location for idle power nor at the 170 and 180 degree locations for all otherpower settings because of turbulent air flow behind the aircraft. Typical A-weighted levels for these angles are 5 to 15dBA below those at the 160 degree location.
* ITest personnel performed noise surveys during quiet periods when the background noise was minimal, e.g., early in themorning when no other aircraft or engine test stands were operating. Data eliminated because they were near thebackground/electronic noise were generally not significant because the levels were so low (e.g., Table 5 at idle power).
Volume 2 of the handbook describes the influence of meteorology on far-field noise environments, and provides, ifrequired, the factors necessary to adjust the handbook's standard meteorological day data.
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26
TABLE 4
TEST CONDITIONSFOR FAR-FIELD NOISE MEASUREMENTS
C-5A Aircraft, Ground Runups, Altus AFB OK14 June 1978Tail #690025
Aircraft Engine Operation
Idle Engine No.. 2 and 3 Only64 % RPM NC (Core Speed)23 % RPM NF Fan Speed)
410 C TIT (Turbine Inlet Temperature)No Register EPR (Engine Pressure Ratio)
1200 LBS/HR FF (Fuel Flow)
1.6 EPR Runup Engine Nos. 2 and 3 Only77 % RPM NC42 %RPM NF
450 C TIT1.60 EPR
2200 LBS/HR FF
2.5 EPR Runup Engine No. 2 and 3 Only85 % RPM NC63 % RPM NF
570 C TIT2.50 EPR
4800 LBS/HR FF
3.5 EPR Runup Engine Nos. 2 and 3 Only90 % RPM NC78 % RPM NF
710 C TIT3.50 EPR8O0 LBS/HR FF
Takeoff Rated Thrust Engine No.. 2 and 3 Only96 % RPM NC90 % RPM NF
810 C TIT4.40 EPR
11000 LBS/HR FF
Meteorology
Temperature 27.8 CBar Pressure 0.727 M HgRel Humidity 54%Wind - Speed 3.6 M/Sec (7 Kts
- Direction 160 Deg
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