Opportunities for supersonic performance gains through non-linear aerodynamics
- 23 July 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Maximum lift-to-drag ratio airfoils at moderate supersonic speeds.AIAA Journal, 1969
- THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDSPublished by Elsevier ,1962
- The Supersonic Conical Wing of Minimum DragJournal of the Aeronautical Sciences, 1955
- A Simplified Two-Dimensional Theory of Thin AirfoilsJournal of the Aeronautical Sciences, 1942