Accession Number : AD0667066

Title :   PRESSURE DISTRIBUTION ON A HYPERSONIC DELTA WING OF DIAMOND CROSS-SECTION,

Corporate Author : DOUGLAS AIRCRAFT CO INC SANTA MONICA CALIF MISSILE AND SPACE SYSTEMS DIV

Personal Author(s) : Ormsbee,A. I.

Report Date : JUL 1967

Pagination or Media Count : 13

Abstract : The work is concerned with the disturbance region associated with a yawed hypersonic delta wing of diamond cross-section. The analysis is presented for zero angle of attack, and it is then shown how angle-of-attack effects may be included. (Author)

Descriptors :   (*DELTA WINGS, HYPERSONIC CHARACTERISTICS), CAMBER, PRESSURE, DISTRIBUTION, GEOMETRIC FORMS, ANGLE OF ATTACK, SHOCK WAVES, YAW, EQUATIONS OF MOTION

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE