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,

Descriptive Note:

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH

Report Date:

1976-10-01

Pagination or Media Count:

45.0

Abstract:

Subject Categories:

  • Fluid Mechanics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE