F-5 Shaped Sonic Boom Demonstrator's Persistence of Boom Shaping Reduction Through Turbulence-Reference-Cited by-同舟云学术

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F-5 Shaped Sonic Boom Demonstrator's Persistence of Boom Shaping Reduction Through Turbulence

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

Author:

Morgenstern John¹,Arslan Alan¹,Lyman Victor¹,Vadyak Joseph¹

Affiliation:

1. Lockheed Martin Aeronautics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-12

Reference19 articles.

1. Sonic‐Boom Minimization

2. Darden,Christine,"SonicBoomMinimizationwithNoseBluntnessRelaxation,"NASATP-1348,1979.

3. 3Carlson, Harry W., Barger, Raymond L., and Mack, Robert J. "Application of Sonic-Boom Minimization Concepts in SupersonicTransportDesign,"NASA TN D-7218, June1973.

4. 4Maglieri, D. J and Bobbitt,P. J. "HistoryofSonicBoomTechnologyincludingminimization"Unpublished and Lockheed Martinproprietary, June27,2001.

5. 5Graham, D., Dahlin, J., Meredith, K., and Vadnais, J. "Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft", AIAA-2005-0008.

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