Accession Number : AD0780337

Title :   Experimental Investigation of a Turbulent Boundary Layer on a Greatly Elongated Body of Revolution in a Supersonic Flow,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kovalenko,V. M. ; Nesterovich,N. I. ; Shulemovich,V. M.

Report Date : 24 MAY 1974

Pagination or Media Count : 12

Descriptors :   *Sounding rockets, *Turbulent boundary layer, Supersonic flow, Bodies of revolution, Wind tunnel models, Translations, USSR

Subject Categories : Rockets
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE