Accession Number : AD0256181

Title :   HYPERSONIC LAMINAR HEAT TRANSFER TO CYLINDRICALLY BLUNTED FLAT PLATES AT ANGLE OF ATTACK

Descriptive Note : Technical rept.,

Corporate Author : GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y

Personal Author(s) : SANLORENZO,ERNEST A.

Report Date : 05 JUL 1960

Pagination or Media Count : 1

Abstract : The objective of this report is to present heat transfer results obtained at M equals 8 in Tunnel B of the von Karman Gas Dynamics Facility, Arnold Engineering Development Center. In addition, theoretical analyses with respect to these results, as performed to date, are presented.

Descriptors :   *BLUNT BODIES, *HEAT TRANSFER, *HYPERSONIC CHARACTERISTICS, *LAMINAR BOUNDARY LAYER, *SUPERSONIC AIRFOILS, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC CONFIGURATIONS, BOUNDARY LAYER, MODEL TESTS, WINGS

Distribution Statement : APPROVED FOR PUBLIC RELEASE