Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail Configuration
- 1 May 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (5) , 297-308
- https://doi.org/10.2514/8.2632