The Supersonic Conical Wing of Minimum Drag
- 1 December 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (12) , 805-817
- https://doi.org/10.2514/8.3476
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Minimum Drag Cambered Rectangular Wing for Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- Slender-Body Theory-Review and ExtensionJournal of the Aeronautical Sciences, 1953
- A Drag Reduction Method for Wings of Fixed Plan FormJournal of the Aeronautical Sciences, 1952
- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951
- Computation of Influence Coefficients for Aircraft Structures with Discontinuities and SweepbackJournal of the Aeronautical Sciences, 1947
- Higher Modes of Vibration by a Method of SweepingJournal of the Aeronautical Sciences, 1946