Missile aerodynamics - Past, present, future
- 17 August 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Vortex development on slender missiles at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Supersonic flow measurements in the body vortex wake of an ogive nose cylinderPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Historical development of world wide guided missilesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Calculation of vortex breakdown locations for flow over delta wingsJournal of Aircraft, 1977
- Dissipation and breakdown of a wing-tip vortexJournal of Fluid Mechanics, 1972
- Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail ConfigurationJournal of the Aeronautical Sciences, 1953
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949
- SUPERSONIC FLOW PAST SLENDER BODIES OF REVOLUTION THE SLOPE OF WHOSE MERIDIAN SECTION IS DISCONTINUOUSThe Quarterly Journal of Mechanics and Applied Mathematics, 1948
- The lift of a delta wing at supersonic speedsQuarterly of Applied Mathematics, 1946
- Supersonic Flow Over an Inclined Body of RevolutionJournal of the Aeronautical Sciences, 1938