Accession Number : AD0092214


Title :   INVESTIGATION AT HIGH SUBSONIC SPEEDS OF SOME EFFECTS OF SIDESLIP ON THE AERODYNAMIC LOADS ON FINNED AND UNFINNED BODIES MOUNTED FROM THE SWEPT-WING OF A WING-FUSELAGE MODEL


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


Personal Author(s) : King, Jr, Thomas J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092214.pdf


Report Date : 26 Apr 1956


Pagination or Media Count : 56


Descriptors :   *LOAD DISTRIBUTION , *WING BODY CONFIGURATIONS , *AIRCRAFT PROTUBERANCES , *FINS , SWEPT WINGS , AERODYNAMIC LOADING , SUBSONIC FLOW , OGIVES


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE