Theoretical prediction of roll moments on finned bodies in supersonic flow
- 30 January 1974
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Aerodynamics of Finned Missiles at High Angle of AttackAIAA Journal, 1971
- ROLL DAMPING MOMENT MEASUREMENTS FOR THE BASIC FINNER AT SUBSONIC AND SUPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1964
- On the Pure Rolling Motion of Winged And/Or Finned Missiles in Varying Supersonic FlightJournal of the Aeronautical Sciences, 1953
- A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling MissileJournal of the Aeronautical Sciences, 1950
- Aerodynamics of thin quadrilateral wings at supersonic speedsQuarterly of Applied Mathematics, 1948