Effects of injection on heat transfer and the boundary-layer instability for a hypersonic blunt body configuration

Author:

Egorov Ivan V.,Palchekovskaya Natalia V.,Obraz Anton O.,Fedorov Alexander V.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference19 articles.

1. Morkovin, M.V., “Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies,” Air Force Flight Dynamics Laboratory, Technical Report AFFDL-TR-68-149, DTIC citation AD-686178, Mar. 1969.

2. Boundary-layer transition with gas injection;Scott;J. Aerospace Sci.,1958

3. Pappas, C.C., and Okuno, A., “Heat-transfer measurement for binary gas laminar boundary layers with high rates of injection,” Ames Research Center, Technical Note TN-D-2473, NASA, Washington, D.C., Sept. 1964. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19640020183.pdf

4. Review and synthesis of roughness-dominated transition correlations for reentry applications;Reda;J. Spacecr. Rockets,2002

5. Hypersonic boundary-layer transition with ablation and blowing;Schneider;J. Spacecr. Rockets,2010

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