Accession Number : AD0745366

Title :   Users Manual for Tilt-Wing and Deflected Slipstream Aerodynamics Program,

Corporate Author : GENERAL DYNAMICS/CONVAIR SAN DIEGO CALIF

Personal Author(s) : Pederson,S. K.

Report Date : 28 MAY 1970

Pagination or Media Count : 54

Abstract : A digital computer program was developed for the purpose of estimating the aerodynamic lift, longitudinal forces and pitching moment characteristics of a tilt-wing or deflected slip-stream V/STOL configuration. Punched card output from this program provides the aerodynamic input data to the performance program for calculating takeoffs, landings and transitions of V/STOL aircraft. (Author)

Descriptors :   (*TILT WINGS, AERODYNAMIC CHARACTERISTICS), SHORT TAKEOFF AIRCRAFT, LIFT, PITCH(MOTION), ANGLE OF ATTACK, CONTROL SEQUENCES, COMPUTER PROGRAMS

Subject Categories : Aerodynamics
      V/STOL
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE