Prediction of Acoustic Loads on a Launch Vehicle: Nonunique Source Allocation Method-Reference-Cited by-同舟云学术

Prediction of Acoustic Loads on a Launch Vehicle: Nonunique Source Allocation Method

Published:2015-09 Issue:5 Volume:52 Page:1478-1485
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Maruf Morshed Mir M.¹,Hansen Colin H.²,Zander Anthony C.²

Affiliation:

1. Department of Mechanical Engineering, Jubail University College, Jubail 31961, Saudi Arabia

2. School of Mechanical Engineering, University of Adelaide, Adelaide, Southern Australia 5005, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33204

Reference21 articles.

1. MayesW. H.LanfordW. E.HubbardH. H. “Near Field and Far Field Noise Surveys of Solid Fuel Rocket Engines for a Range of Nozzle Exit Pressures,” NASA Rept. TN-D-21, 1959.

2. Acoustical Measurements of Static Tests of Clustered and Single‐Nozzled Rocket Engines

3. LassiterL. W.HeitkotterR. H. “Some Measurements of Noise from Three Solid-Fuel Rocket Engines,” NASA Rept. TN-3316, 1954.

4. ColeJ. N.Von GierkeH. E.KyrasisD. T.EldredK. M.HumphreyA. J. “Noise Radiation from Fourteen Types of Rockets in the 1000 to 130,000 Pound Thrust Range,” WADC-Wright Air Development Center, Flight Dynamics Laboratory TR-57-354, Wright–Patterson AFB, OH, 1957.

5. EldredK. M.RobertsW.WhiteR. “Structural Vibrations in Space Vehicles,” WADD-Wright Air Development Division, Flight Dynamics Laboratory TR-61-62, Wright–Patterson AFB, OH, Dec. 1961.

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