Accession Number : AD0228175

Title :   HYPERSONIC SHOCK-LAYER THEORY OF A YAWED CONE AND OTHER THREE-DIMENSIONAL POINTED BODIES

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s) : CHENG, HSIEN K.

Report Date : OCT 1959

Pagination or Media Count : 60

Descriptors :   *CONICAL BODIES, *HYPERSONIC FLOW, BOUNDARY LAYER, MATHEMATICAL ANALYSIS.

Distribution Statement : APPROVED FOR PUBLIC RELEASE