Dynamic stability of a flexible missile under constant and pulsating thrusts
- 1 March 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (3) , 486-494
- https://doi.org/10.2514/3.2891
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Allgemeine Theorie der Stabilität erzwungener Schwingungen elastischer KörperArchive of Applied Mechanics, 1949