Airborne Shaped Sonic Boom Demonstration Pressure Measurements with Computational Fluid Dynamics Comparisons-Reference-Cited by-同舟云学术

Airborne Shaped Sonic Boom Demonstration Pressure Measurements with Computational Fluid Dynamics Comparisons

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Haering Edward¹,Murray James¹,Purifoy Dana¹,Graham David²,Meredith Keith²,Ashburn Christopher³,Stucky Mark⁴

Affiliation:

1. NASA Dryden Flight Research Center

2. Northrop Grumman Corp.

3. Analytical Services & Materials Inc.

4. U.S. Air Force Test Pilot School

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-9

Reference22 articles.

1. 1McLean,F.E."SomeNonasymptoticEffectsontheSonicBoomofLargeAirplanes,"NASATND-2877,1965.

2. 2McLean, F. E., Carlson, H. W., and Hunton, L. W. "Sonic-Boom Characteristics of Proposed Supersonic and Hypersonic Airplanes," NASA TND-3587,1966.

3. Lower bounds for sonic booms in the midfield.

4. Sonic boom minimization including both front and rear shocks

5. Sonic‐Boom Minimization

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