Investigation of Boundary Layer and Performance Effects of Transpiration Cooling through a Porous Plate in a Rocket Nozzle

This study used a range of low blowing ratios with air through an area of porous material in a Mach 2.0 nozzle to quantity the change in boundary layer thickness as a function of blowing ratio. Also, exit and wall Mach number profiles at each blowing ratio were collected to characterize performance...

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Bibliographic Details

Main Author:	Keener, David N.
Format:	text
Published:	AFIT Scholar 1994
Subjects:	Heat > Transmission Rockets (Aeronautics) > Nozzles Porous materials Boundary layer Aerodynamics and Fluid Mechanics
Online Access:	https://scholar.afit.edu/etd/6329 https://scholar.afit.edu/context/etd/article/7332/viewcontent/AFIT_GA_ENY_94D_3_Keener_D_ADA289393_Redacted.pdf
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