Design of Missile Bodies for Minimum Drag at Very HIgh Speeds -- Thickness Ratio, Lift, and Center of Pressure Given
- 1 September 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (9) , 568-570
- https://doi.org/10.2514/8.8205
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Drag Coefficient of Very High Velocity SpheresJournal of the Aeronautical Sciences, 1957
- Lift on Inclined Bodies of Revolution in Hypersonic FlowJournal of the Aeronautical Sciences, 1950
- The Linearized Subsonic and Supersonic Flow About Inclined Slender Bodies of RevolutionJournal of the Aeronautical Sciences, 1947