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Factors Affecting Transition at Supersonic Speeds

K. R. Czarnecki

出版	National Advisory Committee for Aeronautics, 1953
URL	http://books.google.com.hk/books?id=QIQ7C9cbRNMC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

This paper surveys the available material and summarizes what is known to date about boundary-layer transition at supersonic speeds. Variables studied include Mach number, Reynolds number, pressure gradients, heat transfer, surface roughness, and angle of attack. The discussion is limited to bodies of revolution because similar reliable data for wings is lacking.