Accession Number:

AD0802293

Title:

AERODYNAMIC FORCE ANALYSIS. VOLUME I

Descriptive Note:

Corporate Author:

AUBURN UNIV AL DEPT OF AEROSPACE ENGINEERING

Personal Author(s):

Report Date:

1966-06-30

Pagination or Media Count:

523.0

Abstract:

Aerodynamic Force Analysis methods and technology from an extensive bibliography, originally prepared as an internal reference for the U. S. Army Missile Command, is presented in conjunction with definitive guidance for use and applicability. An altitude range from 0 to 400,000 feet and a Mach number range from low subsonic through oribital-re-entry level hypersonic is encompassed, with appropriate continuum, slip and free molecule flow treatments.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE