Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed-Reference-Cited by-同舟云学术

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Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed

Published:2005-03 Issue:3 Volume:17 Page:036102
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Sahoo Niranjan,Kulkarni Vinayak,Saravanan S.,Jagadeesh G.,Reddy K. P. J.

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/1.1862261

Reference21 articles.

1. High-speed aerodynamics of several blunt-cone configurations

2. Hypersonic convective heat transfer over 140-deg blunt cones in different gases

3. High-Enthalpy Aerothermodynamics of a Mars Entry Vehicle Part 1: Experimental Results

4. L. D. Huebner, A. M. Mitchell, and E. J. Boudreaux, “Experimental results on the feasibility of an aerospike for hypersonic missiles,” AIAA Pap. 95–0737, 1995.

5. Numerical investigation of supersonic flows around a spiked blunt body

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