Advances in Supersonic Configuration Design Methods
- 1 February 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (2) , 119-126
- https://doi.org/10.2514/3.57882
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Aerodynamic Design of a Mach 2.2 Supersonic Cruise AircraftJournal of Aircraft, 1978
- Three-dimensional canard-wing shape optimization in aircraft cruise and maneuver environmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- An improved higher order panel method for linearized supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Aircraft aerodynamic design and evaluation methodsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex ConfigurationsAIAA Journal, 1975
- Readers ForumJournal of the Aerospace Sciences, 1959
- The Kutta Condition and the Condition for Minimum DragJournal of the Aerospace Sciences, 1959
- On Jones' Criterion for Optimum Lifting WingsJournal of the Aerospace Sciences, 1958
- On Optimum Thin Lifting Surfaces at Supersonic SpeedsJournal of the Aerospace Sciences, 1958
- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951