Transition Effects on Slender Vehicle Stability and Trim Characteristics
- 1 January 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (1) , 3-11
- https://doi.org/10.2514/3.61996
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
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