Publication Date:
2019-07-13
Description:
A summary is provided of an experimental investigation which was carried out to determine the cooling effectiveness of an injection of water through slotted and porous surfaces into a turbulent, supersonic boundary layer. Correlations, based on the experimental data and the supporting analysis, were incorporated into a computer-code model. The model is used to compute discrete injection coolant flow rate requirements for arbitrary slot sizes and heating environments.
Keywords:
FLUID MECHANICS
Type:
AIAA PAPER 74-98
,
Aerospace Sciences Meeting; Jan 30, 1974 - Feb 01, 1974; Washington, DC
Format:
text
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