High speed flight effects on noise propagation
Author:
Affiliation:
1. Lockheed-Georgia Co., Marietta
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-13
Reference10 articles.
1. R. H. Burrin, K. K. Ahuja, and M. Salikuddin, 1986 AFWALO-TR-86 to be assigned. High speed flight effects on noise propagation.
2. H. Salikuddin. P. D. Dean. H. E. Plumblee. Jr., and K. K.' Ahuja 1980 Journal of Sound an'd Vibration 70, 487-501. An impulse test technique vith application to acoustic measurements.
3. H. Salikuddin, K. K. Ahuja, and W. H. Brown 1984 Journal of Sound and Vibration 94,33-61. An improved impulse method for studies on acoustic transmission in flav ducts vith use of signal synthesis and averaging of acoustic pulses.
4. K. K. Ahuja, M. Salikuddin, R. H. Burrin and H. E. Plumblee, Jr. 1980 NASA CR-165144. A study of the acoustic transmission characteristics of suppressor nozzles.
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1. High speed flight effects on noise propagation;25th AIAA Aerospace Sciences Meeting;1987-03-24
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