Accession Number:

AD0069271

Title:

ESTIMATED AERODYNAMIC CHARACTERISTICS FOR DESIGN OF THE F-86E AIRPLANE

Descriptive Note:

Corporate Author:

NORTH AMERICAN AVIATION INC LOS ANGELES CA

Personal Author(s):

Report Date:

1950-12-26

Pagination or Media Count:

121.0

Abstract:

This report is a compilation of aerodynamic data for design of the F-86E airplane. The aerodynamic coefficients presented herein are based on wind tunnel tests conducted in the North American Aerodynamics laboratory 7.75 x 11 foot low speed wind tunnel and in the high speed Southern California Cooperative Wind Tunnel. NACA experimental results are also utilized.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE