Accession Number:

AD0251555

Title:

THE SHOCK LAYER CONCEPT AND THREE-DIMENSIONAL HYPERSONIC BOUNDARY LAYERS

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

Report Date:

1961-01-01

Pagination or Media Count:

33.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE