Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures from 1,295 degrees F to 2,910 degrees F /
by Bernard Rashis.
|Main Author:||Rashis, Bernard.|
Washington, D.C. : National Aeronautics and Space Administration : 
Aerodynamics, missiles and space vehicles.
Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mechanics.
Supersedes NACA RM L57F11
18 p. :
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|Full view||University of Illinois at Urbana-Champaign|