Accession Number : AD0617421

Title :   THE FLOW OVER A WEDGE PROFILE AT MACH NUMBER ONE,

Corporate Author : AIR MATERIEL COMMAND WRIGHT-PATTERSON AFB OHIO ENGINEERING DIV

Personal Author(s) : Guderley,Gottfried ; Yoshihara,Hideo

Report Date : JUL 1949

Pagination or Media Count : 45

Abstract : The flow over a wedge-shaped profile at zero angle of attack and with a free stream Mach number of one is computed using the hodograph method as simplified by the transonic law of similarity. Drag coefficients are computed for several profiles. (Author)

Descriptors :   (*WEDGES, TRANSONIC FLOW), (*TRANSONIC FLOW, WEDGES), DRAG, ANGLE OF ATTACK, NUMERICAL ANALYSIS, BOUNDARY VALUE PROBLEMS

Distribution Statement : APPROVED FOR PUBLIC RELEASE