Accession Number : AD0010714


Title :   SUBSONIC STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A WING-BODY COMBINATION HAVING A POINTED WING OF ASPECT RATIO 2 WITH CONSTANT-PERCENT-CHORD TRAILING-EDGE ELEVONS


Descriptive Note : Research memo.


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


Personal Author(s) : SMITH, DONALD W ; REED, VERLIN D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/010714.pdf


Report Date : 22 May 1953


Pagination or Media Count : 157


Descriptors :   *WINGS , *ELEVONS , PITCH(MOTION) , FUSELAGES


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE