Accession Number : AD0029198


Title :   FLIGHT INVESTIGATION OF THE EFFECTS OF A PARTIAL-SPAN LEADING-EDGE CHORD EXTENSION ON THE AERODYNAMIC CHARACTERISTICS OF A 35 deg SWEPT-WING FIGHTER AIRPLANE


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER


Personal Author(s) : Matteson, Frederick H ; Van Dyke, Jr, Rudolph D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/029198.pdf


Report Date : 23 Apr 1954


Pagination or Media Count : 39


Descriptors :   *AERODYNAMIC CHARACTERISTICS , *SWEPTBACK WINGS , JET AIRCRAFT , JET FIGHTERS , PITCH(MOTION) , FIGHTER AIRCRAFT


Subject Categories : Aircraft
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE