Alterations in Critical Radii of Bluntness of Shock Wave Boundary Layer Interaction

Author:

John Bibin1,Kulkarni Vinayak2

Affiliation:

1. Associate Professor, School of Mechanical and Building Sciences, VIT Univ., Near Katpadi Rd., Vellore, Tamil Nadu 632014, India.

2. Associate Professor, Dept. of Mechanical Engineering, IIT Guwahati, Guwahati, Assam 781039, India (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference21 articles.

1. On the influence of elevated surface temperatures on hypersonic shock wave/boundary layer interaction at a heated ramp model

2. Chapman D. R. Kuehn D. M. and Larson H. K. (1957). “Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition.” NACA Rep. 1356 National Advisory Committee for Aeronautics Moffett Field CA.

3. Experiments on shock wave/boundary layer interaction in hypersonic flow;Coët M.;La Recherche Aerospatiale,1993

4. Entropy-layer instabilities over a blunted flat plate in supersonic flow

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