Experiments conducted in supersonic wind tunnels during past 3 yr on missiles and projectiles show that pressure at base of bodies is essentially function of parameters that govern boundary layer; hence, base pressure is closely connected to surface friction and heat transfer phenomena; experimental results obtained in Naval Ordnance Laboratory supersonic tunnels at Mach 1.5-5.0 compared with theoretical results.
Interrelationship between boundary layer and base pressure
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 11
1951
6 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Interrelationship between ship and diesel engine
IOS Press | 1958
|Interrelationship between Airport Enplanements and Accessibility
Transportation Research Record | 2019
|Boundary-layer thickness and base pressure
AIAA | 1985
|Interrelationship between ship and diesel engine
Engineering Index Backfile | 1958
|Interrelationship Between Airport Enplanements and Accessibility
Online Contents | 2015
|