Accession Number : ADA298764

Title :   Stability Derivatives of Triangular Wings at Supersonic Speeds,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER

Personal Author(s) : Ribner, Herbert S. ; Malvesstuto, Frank S., Jr

PDF Url : ADA298764

Report Date : 1948

Pagination or Media Count : 15

Descriptors :   *AERODYNAMIC STABILITY, *SUPERSONIC CHARACTERISTICS, PRESSURE GRADIENTS, PITCH(MOTION), YAW, MOMENTS, ANGLE OF ATTACK, SUBSONIC CHARACTERISTICS, MACH NUMBER, UNSTEADY FLOW, SUPERSONIC FLOW, PRESSURE DISTRIBUTION, AERODYNAMIC LIFT, ASPECT RATIO, POTENTIAL FLOW.

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE