Aerodynamics of Finned Missiles at High Angle of Attack
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (12), 2378-2384
- https://doi.org/10.2514/3.50043
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Supersonic magnus effect on a finned missileAIAA Journal, 1964
- A theory of the flow past a slender delta wing with leading edge separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959
- Dynamic Stability of a Missile in Rolling FlightJournal of the Aeronautical Sciences, 1952