Numerical Solution of the Supersonic and Hypersonic Viscous Flow around Thin Delta Wings
- 1 September 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (9) , 942-949
- https://doi.org/10.2514/3.61256
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Computation of three-dimensional, inviscid supersonic flowsPublished by Springer Nature ,2008
- Flow Regimes over Delta Wings at Supersonic and Hypersonic SpeedsAeronautical Quarterly, 1976
- A survey of leeside flow and heat transfer on delta planform configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- A numerical study of supersonic viscous cone flow at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Lee-side vortices on delta wings at hypersonic speeds.AIAA Journal, 1972
- Supersonic and hypersonic flow with attached shock waves over delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1971
- Some experiments on delta wings in hypersonic flow.AIAA Journal, 1966
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964
- Numerical solution of the problem of flow round the upper surface of a triangular wing by a supersonic streamUSSR Computational Mathematics and Mathematical Physics, 1963
- Exact and Approximate Solutions for the Supersonic Delta WingJournal of the Aeronautical Sciences, 1956