The Incorporation of Plotting Capability Into the "unified Subsonic Supersonic Aerodynamic Analysis Program", Version BNational Aeronautics and Space Administration, Scientific and Technical Information Office, 1980 - Aerodynamics - 137 pages |
Common terms and phrases
airfoil leading edge ALPHA angle of attack Array containing block matrices BODPAN BODVEL body panel body segment boundary condition calculated camber canard column of panels Columns Variable Value computes CONFIG configuration CONPLT consists of program Control integer data coordinate system define definition parameter dihedral angle FORMOM FUSELAGE PRESSURE fuselage segment GEOM geometry data GPLTSV identified in columns inclination angles ITRATE KCAN KFINOR KFORX KRADX LINVEL MACH matrix NACA NEWORD NFORX normal velocity NRADX Number of ordinates Number of points OTHPLT output overlay consists Overlay LWB overlay programs panel control points panel corner points panel edges partition percent chord PLTORT point coordinates point in data pressure coefficients pressure distribution print option reading plot cards singularity paneling source and vortex SPPLT subroutine TALPAN TAPE 9 trailing edge TRANSONIC unit vectors USSAERO VELCMP velocity components induced view point WAFORD wing panels WNGPAN WNGVEL written on TAPE X-coordinate Y-origin on paper Yaw angle