Quiet Spike Prototype Flight Test Results
Author:
Affiliation:
1. Gulfstream Aerospace Corporation
2. NASA Dryden Flight Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1778
Reference6 articles.
1. Howe,D.C. "Improved Sonic BoomMinimizationwith ExtendableNoseSpike",AIAA-2005-1014.
2. Howe, D.C. "Sonic Boom Reduction Through The Use Of Non-Axsymmetric Configuration Shaping", AIAA-2003-0929.
3. Simmons III, F., Freund, D., Spivey, N. D., and Schuster, L. "Quiet Spike™: The Design and Validation ofanExtendableNoseBoomPrototype,"AIAA-2007-1774(tobepublished).
4. Spivey, N. etal, "Quiet Spike Build-Up Ground Vibration Testing Approach", AIAA-2007-1175 (to be published).
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