Integral Approximation for Slender-Body Shock Shapes in Hypersonic Flow

The investigation reported is concerned with a method due to Chernyi (1961). Chernyi arrives at a pair of ordinary differential equations which describe the shock shapes and body pressure distribution associated with slender planar bodies and bodies of revolution. The investigation shows that the pa...

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Veröffentlicht in:AIAA journal 1974-12, Vol.12 (12), p.1735-1737
Hauptverfasser: FIORINO, THOMAS D., RASMUSSEN, MAURICE L.
Format: Artikel
Sprache:eng
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