Accession Number : AD0782202

Title :   A Computer Program for Three-Dimensional Lifting Bodies in Subsonic Inviscid Flow.

Descriptive Note : Final rept.,

Corporate Author : FLOW RESEARCH INC KENT WASH

Personal Author(s) : Woodward,F. A. ; Dvorak,F. A. ; Geller,E. W.

Report Date : APR 1974

Pagination or Media Count : 147

Abstract : A computer program for the analysis of wing-body combinations in subsonic flow is described. The configuration is represented by a large number of surface panels. The circulation about lifting surfaces is provided by a system of vortex lattices. The strengths of the sources and vortices which satisfy the boundary condition of tangential flow for a given Mach number, angle of attack, and/or angle of yaw are determined by solving a system of linear equations by an iterative procedure. The program computes the pressure coefficients at the panel centroids and integrates these pressures numerically to obtain the lift, drag, and pitching moments. (Modified author abstract)

Descriptors :   *WING BODY CONFIGURATIONS, *AERODYNAMIC CHARACTERISTICS, *COMPUTER PROGRAMS, LIFTING BODIES, THREE DIMENSIONAL FLOW, SUBSONIC CHARACTERISTICS, INVISCID FLOW, VORTICES, ANGLE OF ATTACK, YAW, MATHEMATICAL MODELS, PRESSURE, COEFFICIENTS, NUMERICAL METHODS AND PROCEDURES, EQUATIONS OF MOTION, FORTRAN

Subject Categories : Computer Programming and Software
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE