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Wind Tunnel Simulation of Head-on Bow Wave-blast Wave Interactions
David L. Merritt
P. M. Aronson
出版
United States Naval Ordnance Laboratory
, 1967
URL
http://books.google.com.hk/books?id=qACg8jKAWigC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
A unique wind tunnel - shocktube technique for simulating the head-on interaction between a supersonic vehicle and a blast wave is described. The technique is verified by comparing theory with pressure measurements from a wedge and a hemisphere. Overpressure data are presented for a slender cone at angles of attack up to 10 degrees. (Author).
