Aerodynamic shape optimization of hypersonic missiles
- 17 August 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Study of the shock system for flow past star-shaped bodiesFluid Dynamics, 1966
- Nose Shape for Minimum Drag in Hypersonic FlowJournal of the Aerospace Sciences, 1962
- Design of Missile Bodies for Minimum Drag at Very HIgh Speeds -- Thickness Ratio, Lift, and Center of Pressure GivenJournal of the Aerospace Sciences, 1959