Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes

By V. Menezes, S. Saravanan, G. Jagadeesh, K. Reddy. 2003

142 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/27ec4b51c0479e4a94a973c5c97499d0fecf25fa

Citations in the corpus

• Numerical analysis on cooling performance of counterflowing jet over aerodisked blunt body (2014, unknown): “The geometry of the nose cone is assumed to have the same size and shape as the experimentally investigated structure of [4].”