Slot injection problems include fuel injection, surface cooling and/ or skin-friction reduction, and alleviation of boundary-layer separation by energizing fluid near wall; study is divided into three areas; detailed profiles in near flowfield were determined with interferometer for air injection into Mach 2.1 airstream past flat plate; analytical treatment of turbulent mixing zone including effects of splitter plate boundary layer is presented and shown to provide predictions in excellent agreement with experiments; stability of mixing region is considered and experiments with spark shadowgraphs are reported.
Tangential slot injection in supersonic flow
AIAA J
AIAA Journal ; 5 , n 12
1967
6 pages
Article (Journal)
English
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Tangential slot injection in supersonic flow.
AIAA | 1967
|Tangential slot injection in supersonic flow
AIAA | 1967
|