The role of constraints in the inverse design problem for transonic airfoils
- 23 June 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Artificial viscosity method for the design of supercritical airfoils. [Analysis code H]Published by Office of Scientific and Technical Information (OSTI) ,1979
- Transonic Airfoil Analysis and Design Using Cartesian CoordinatesJournal of Aircraft, 1976
- Exact Method of Designing Airfoils With Given Velocity Distribution in Incompressible FlowJournal of Aircraft, 1973
- The design of two-dimensional aerofoils with mixed boundary conditionsQuarterly of Applied Mathematics, 1955
- The Behavior at Infinity of The Potential Function of a Two Dimensional Subsonic Compressible FlowJournal of Mathematics and Physics, 1951