Experimental Verification of Buffet Calculation Procedure Using Unsteady Pressure-Sensitive Paint
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033917
Reference20 articles.
1. Design and verification of launch and space vehicle structures
2. ColeH. A.EricsonA. L.RaineyA. G. “Buffeting During Atmospheric Ascent, NASA Space Vehicle Design Criteria (Structures),” NASA SP-8001, May 1964, rev. Nov. 1970.
3. Vibration response of spacecraft shrouds toin-flight fluctuating pressures
4. Ares Launch Vehicle Transonic Buffet Testing and Analysis Techniques
5. Estimation of the Unsteady Aerodynamic Load on Space Shuttle External Tank Protuberances from a Component Wind Tunnel Test
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