Boundary Layer Investigation in the Impingement Area of Rocket Engine Blast.
Final rept. Dec 65-Jul 66,
ARMY ENGINEER WATERWAYS EXPERIMENT STATION VICKSBURG MISS
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The purpose of the investigation was to Study the boundary layer when rocket exhaust gases discharge in open air and impinge on variously shaped surfaces. Determine the feasibility of controlling the blast effects by using a boundary layer of ambient air to prevent excessive heat transfer from the exhaust gas to the surface of the blast-control medium. Author
- Guided Missile Launching and Basing Support