Accession Number : AD0613463

Title :   SEPARATED FLOW STUDIES AT HYPERSONIC SPEEDS. PART II. TWO-DIMENSIONAL WEDGE SEPARATED FLOW STUDIES,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Holden,Michael

Report Date : DEC 1964

Pagination or Media Count : 70

Abstract : The paper describes an experimental study of the flow patterns and distribution of heat transfer developed in regions of adverse pressure gradient and separated flow over two-dimensional models. The investigation was directed towards obtaining information on two basic problems, the separation and the reattachment of a laminar boundary layer.

Descriptors :   (*HYPERSONIC FLOW, SEPARATION), (*WEDGES, TWO DIMENSIONAL FLOW), (*HEAT TRANSFER, AERODYNAMIC CONFIGURATIONS), AERODYNAMIC HEATING, SHOCK WAVES, LAMINAR BOUNDARY LAYER, FLAT PLATE MODELS, SCHLIEREN PHOTOGRAPHY, MEASUREMENT

Distribution Statement : APPROVED FOR PUBLIC RELEASE