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