User instructions for the Tektronix Graphics Package of the Automated Paneling Technique (APT) and the Wing and Body Aerodynamic Technique (WABAT) Programs are provided. Responses to plot package messages which the user must make to activate plot package operations and options are described. Modifications to the APT and WABAT input run streams, to affect the graphic interface, are also covered
An integrated system of computer programs for supersonic configurations is described. An explanation...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...
User instructions for a graphics package for coupled rotor/airframe vibration analysis are presented...
A description of and users manual for a USA FORTRAN IV computer program which plots the planform and...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
Computer programs to produce the ordinates for airfoils of any thickness, thickness distribution, or...
The latest production version, MARK IV, of the NASA-Langley vortex lattice computer program is summa...
PLOT3D is a computer graphics program designed to visualize the grids and solutions of computational...
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are sum...
The computer program documentation for the design and analysis of supersonic configurations is prese...
A method of developing an input data file for use in the aerodynamic analysis of a complete airplane...
The B01 version of the United Subsonic Supersonic Aerodynamic Analysis program is the result of nume...
A three dimensional transonic Wind-tunnel Interference Assessment and Correction (WIAC) procedure de...
An integrated system of computer programs for supersonic configurations is described. An explanation...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...
User instructions for a graphics package for coupled rotor/airframe vibration analysis are presented...
A description of and users manual for a USA FORTRAN IV computer program which plots the planform and...
The Rotor-Fuselage Analysis is a method of calculating the aerodynamic reaction between a helicopter...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
Computer programs to produce the ordinates for airfoils of any thickness, thickness distribution, or...
The latest production version, MARK IV, of the NASA-Langley vortex lattice computer program is summa...
PLOT3D is a computer graphics program designed to visualize the grids and solutions of computational...
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are sum...
The computer program documentation for the design and analysis of supersonic configurations is prese...
A method of developing an input data file for use in the aerodynamic analysis of a complete airplane...
The B01 version of the United Subsonic Supersonic Aerodynamic Analysis program is the result of nume...
A three dimensional transonic Wind-tunnel Interference Assessment and Correction (WIAC) procedure de...
An integrated system of computer programs for supersonic configurations is described. An explanation...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...