Supersonic and hypersonic flow with attached shock waves over delta wings
- 9 November 1971
- journal article
- Published by The Royal Society in Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences
- Vol. 325 (1561) , 251-268
- https://doi.org/10.1098/rspa.1971.0168
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Stability of oscillating wedges and caret wings in hypersonic and supersonic flows.AIAA Journal, 1969
- Calculated Pressure Distributions and Shock Shapes on Conical Wings with Attached Shock WavesAeronautical Quarterly, 1968
- Hypersonic flow over a delta wing of moderate aspect ratio.AIAA Journal, 1966
- NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WINGAIAA Journal, 1963
- LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORYAIAA Journal, 1963
- The diffraction of blast. IIProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1950