Transition effects on slender vehicle stability and trim characteristics
Author:
Affiliation:
1. Lockheed Missiles and Space, Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-126
Reference97 articles.
1. Oct. 1963.
2. Ablation effects on vehicle dynamics.
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1. Investigation on Dynamic Derivative Test Technique in Hypersonic Wind Tunnel;Lecture Notes in Electrical Engineering;2019
2. Effect of nose bluntness and cone angle on slender-vehicle transition;AIAA Journal;1988-10
3. Analysis of Re-Entry Vehicle Behavior during Boundary-Layer Transition;AIAA Journal;1975-02
4. Entropy gradient effects on blunted cone transition;13th Aerospace Sciences Meeting;1975-01-20
5. Transition Effects on Slender Vehicle Stability and Trim Characteristics;Journal of Spacecraft and Rockets;1974-01
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