Transition Effects on Slender Vehicle Stability and Trim Characteristics
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.61996
Reference40 articles.
1. Influence of ablation on the dynamics of slender re-entry configurations
2. Ablation effects on vehicle dynamics.
3. Effect of boundary-layer transition on vehicle dynamics
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