Accession Number:

ADA278326

Title:

Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CENTER

Personal Author(s):

Report Date:

1953-01-01

Pagination or Media Count:

15.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE