Accession Number : AD0011100


Title :   LOADS EXPERIENCED IN FLIGHTS OF TWO SWEPT-WING RESEARCH AIRPLANES IN THE ANGLE-OF-ATTACK RANGE OF REDUCED STABILITY


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : DRAKE, HUBERT M ; ROBINSON, GLENN H ; KUHL, ALBERT E


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/011100.pdf


Report Date : 05 Jun 1953


Pagination or Media Count : 14


Descriptors :   *LOAD DISTRIBUTION , *SWEPT WINGS , STABILITY


Subject Categories : Aircraft
      Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE