Conical, noncircular, second-order, potential theory of supersonic flow
- 1 May 1984
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (5) , 618-623
- https://doi.org/10.2514/3.8646
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Approximate factorization schemes for 3D nonlinear supersonic potential flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- EULER SOLUTIONS OF SUPERSONIC WING-BODY INTERFERENCE AT HIGH INCIDENCE INCLUDING VORTEX EFFECTSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Finite area method for nonlinear conical flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Supersonic Inviscid Flowfield Computations of Missile Type BodiesAIAA Journal, 1981
- PAN AIR - A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical Procedure for the Computation of Irrotational Conical FlowsAIAA Journal, 1979
- Improved Wave Drag Predictions Using Modified Linear TheoryJournal of Aircraft, 1979
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951