Accession Number : AD0251555

Title :   THE SHOCK LAYER CONCEPT AND THREE-DIMENSIONAL HYPERSONIC BOUNDARY LAYERS

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s) : CHENG, HSIEN K.

Report Date : JAN 1961

Pagination or Media Count : 33

Descriptors :   *HYPERSONIC CHARACTERISTICS, *HYPERSONIC FLOW, *LAMINAR BOUNDARY LAYER, CONICAL BODIES, SHEETS, SHOCK WAVES, THEORY, YAW.

Distribution Statement : APPROVED FOR PUBLIC RELEASE