Dynamic Stability of a Missile in Rolling Flight
- 1 June 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (6) , 395-403
- https://doi.org/10.2514/8.2308
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling MissileJournal of the Aeronautical Sciences, 1950
- On the motion of a spinning shellQuarterly of Applied Mathematics, 1946
- X. The aerodynamics of a spinning shellPhilosophical Transactions of the Royal Society A, 1921