Accession Number : AD0650960
Title : SUPERSONIC GAS FLOW PAST A CYLINDRICAL PROTUBERANCE OF A PLATE.
Descriptive Note : APL library bulletin translations series,
Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Personal Author(s) : Voitenko,D. M. ; Zubkov,A. I. ; Panov,Yu. A.
Report Date : 31 JAN 1967
Pagination or Media Count : 13
Abstract : Wind-tunnel investigation was made of the flow past a cylindrical protuberance on a plate at a Mach number of 2.5. The shape of the separation line and the pressure distribution and flow orientation at the surface of the plate, obtained for cylinders of various diameter and height, are presented in graphical form. (Author)
Descriptors : (*CYLINDRICAL BODIES, *SUPERSONIC FLOW), FLOW SEPARATION, PRESSURE, FLOW FIELDS, WIND TUNNEL MODELS, LEADING EDGES, VORTICES, USSR, THREE DIMENSIONAL FLOW
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE