2 Result(s)
within
Chapter
S. Mohammed Ibrahim
Aerospace Technology and Astronautics
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Chapter and Conference Paper
Reynolds Number Effects on Shock Wave Boundary Layer Interaction in a Hypersonic Flow
The Reynolds number is found to affect the separation bubble for shock im**ement locations away from the leading edge where finite separation occurs. A decrease in separation bubble was observed with an incr...
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Chapter and Conference Paper
Experimental Investigation of Film Cooling Technique over a Blunt Body in Hypersonic Flow
As an alternative to conventional TPS (thermal protection system), film cooling technique has been previously extensively studied. The aim of the current work is to inject new coolants, i.e., mist (atomized wa...
