Ground Measurements of a Shaped Sonic Boom-Reference-Cited by-同舟云学术

Ground Measurements of a Shaped Sonic Boom

Published:2004-05-10 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Plotkin Kenneth¹,Page Juliet¹,Graham David²,Pawlowski Joseph²,Schein David²,Coen Peter³,McCurdy David³,Haering Edward⁴,Maglieri Domenic⁵,Pilon Anthony⁶,Salamone Joe⁷,Murray James⁴,Ehernberger L⁴,Bobbitt Percy⁸

Affiliation:

1. Wyle Laboratories

2. Northrop-Grumman Corporation

3. NASA Langley Research Center

4. NASA Dryden Flight Research Center

5. Eagle Aeronautics Inc

6. Lockeed Martin Aeronautics Company

7. Gulfstream Aerospace Corporation

8. Eagle Aeronautics, Inc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2923

Reference15 articles.

1. The flow pattern of a supersonic projectile

2. Design Methods for Minimization of Sonic‐Boom Pressure‐Field Disturbances

3. Sonic boom minimization including both front and rear shocks

4. Some Effects of Applying Sonic Boom Minimization to Supersonic Cruise Aircraft Design

5. 5McLean,F.Edward,"SomeNonasymptoticEffectsontheSonicBoomofLargeAirplanes,"NASATND-2877,June1965.

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