Accession Number : ADA955903

Title :   A Comparison of Wind Tunnel Data and Theoretical Predictions at M = 2.30, 2.60, and 2.96 for a Fighter with a Wing Having 74 Degrees of Sweep,

Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH

Personal Author(s) : Sotomayer, William A. ; Weeks, Thomas M.

Report Date : OCT 1976

Pagination or Media Count : 45

Descriptors :   *SUPERSONIC CHARACTERISTICS, SUPERSONIC AIRCRAFT, AERODYNAMIC FORCES.

Subject Categories : Fluid Mechanics
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE