Prediction of Scattered Broadband Shock-Associated Noise-Reference-Cited by-同舟云学术

Prediction of Scattered Broadband Shock-Associated Noise

Published:2016-01 Issue:1 Volume:54 Page:343-359
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Miller Steven A. E.¹

Affiliation:

1. Aeroacoustics Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054280

Reference51 articles.

1. Toward a Comprehensive Model of Jet Noise Using an Acoustic Analogy

2. MillerS. A. E. “The Prediction and Analysis of Jet Flows and Scattered Turbulent Mixing Noise About Flight Vehicle Airframes,” NASA TM-2014-218506, 2014.

3. YuJ. C. “Investigation of the Noise Field of Supersonic Axisymmetric Jet Flow,” Ph.D. Dissertation, Syracuse Univ., Syracuse, NY, 1971.

4. TannaH. K.DeanP. D.BurrinR. H. “The Generation and Radiation of Supersonic Jet Noise. Volume 4. Shock-Associated Noise Data,” U.S. Air Force Aero Propulsion Lab. TR-76-65, Wright-Patterson AFB, OH, 1976.

5. Experiments of shock associated noise of supersonic jets

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