Accession Number : AD0096084


Title :   PHASE IV PERFORMANCE TEST OF THE F-86F-40 AIRPLANE EQUIPPED WITH 6 X 3-INCH LEADING EDGE SLATS AND 12-INCH EXTENSIONS ON THE WING TIPS


Corporate Author : AIR FORCE FLIGHT TEST CENTER EDWARDS AFB CA


Personal Author(s) : HANKS, NORRIS J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/096084.pdf


Report Date : May 1956


Pagination or Media Count : 56


Descriptors :   *JET FIGHTERS , STABILITY


Subject Categories : Aircraft
      Attack and Fighter Aircraft
      Test Facilities, Equipment and Methods


Distribution Statement : APPROVED FOR PUBLIC RELEASE