Transonic Inviscid Flow over Lifting Airfoils by the Method of Integral Relations
- 1 June 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (6), 798-804
- https://doi.org/10.2514/3.49353
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Subcritical flows over two dimensional airfoils by a multistrip method of integral relationsPublished by Springer Nature ,2008
- The calculation of high subsonic flow past bodies by the method of integral relationsPublished by Springer Nature ,2008
- Computation of Transonic Flows past Lifting Airfogs and Slender BodiesAIAA Journal, 1972
- Theory of Exhaust-Plume/Boundary-Layer Interactions at Supersonic SpeedsAIAA Journal, 1972
- Transonic Flow about Two-Dimensional Airfoils by Relaxation ProceduresAIAA Journal, 1972
- NUMERICAL DESIGN OF TRANSONIC AIRFOILS**The work presented in this paper is supported by the AEC Computing and Applied Mathematics Center, Courant Institute of Mathematical Sciences, New York University, under Contract AT(30-1)-1480 with the U. S. Atomic Energy Commission.Published by Elsevier ,1971
- Calculation of plane steady transonic flowsAIAA Journal, 1971
- Inviscid transonic flow over airfoilsAIAA Journal, 1970
- Structure of Weak Non-Hugoniot ShocksPhysics of Fluids, 1963
- On the Prediction of Mixed Subsonic/Supersonic Pressure DistributionsJournal of the Aerospace Sciences, 1960