Accession Number : AD0069271


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


Corporate Author : NORTH AMERICAN AVIATION INC LOS ANGELES CA


Personal Author(s) : GARDNER, F T ; DOWNEY, H T


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/069271.pdf


Report Date : 26 Dec 1950


Pagination or Media Count : 121


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.


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *JET FIGHTERS , EXPERIMENTAL DATA , WIND TUNNEL TESTS


Subject Categories : Attack and Fighter Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE