The B01 version of the United Subsonic Supersonic Aerodynamic Analysis program is the result of numerous modifications and additions made to the B00 version. These modifications and additions affect the program input, its computational options, the code readability, and the overlay structure. The following are described: (1) the revised input; (2) the plotting overlay programs which were also modified, and their associated subroutines, (3) the auxillary files used by the program, the revised output data; and (4) the program overlay structure
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A user/programmer manual for the computer program SOUSSA P 1.1 is presented. The program was designe...
Aerodynamics calculations are treated in routines which concern moments as they vary with flight con...
The computer program documentation for the design and analysis of supersonic configurations is prese...
Versions B and C of the unified subsonic and supersonic aerodynamic analysis program, USSAERO, are d...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
An integrated system of computer programs for supersonic configurations is described. An explanation...
A description of and users manual for a USA FORTRAN IV computer program which plots the planform and...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are sum...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The AEROX program estimates lift, induced-drag and pitching moments to high angles (typ. 60 deg) for...
An integrated system of computer programs has been developed for the design and analysis of superson...
An aerodynamic analysis system based on potential theory at subsonic and/or supersonic speeds and im...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A user/programmer manual for the computer program SOUSSA P 1.1 is presented. The program was designe...
Aerodynamics calculations are treated in routines which concern moments as they vary with flight con...
The computer program documentation for the design and analysis of supersonic configurations is prese...
Versions B and C of the unified subsonic and supersonic aerodynamic analysis program, USSAERO, are d...
Sufficient instructions for running the subsonic/supersonic advanced panel pilot code were developed...
An integrated system of computer programs for supersonic configurations is described. An explanation...
A description of and users manual for a USA FORTRAN IV computer program which plots the planform and...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are sum...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The AEROX program estimates lift, induced-drag and pitching moments to high angles (typ. 60 deg) for...
An integrated system of computer programs has been developed for the design and analysis of superson...
An aerodynamic analysis system based on potential theory at subsonic and/or supersonic speeds and im...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A user/programmer manual for the computer program SOUSSA P 1.1 is presented. The program was designe...
Aerodynamics calculations are treated in routines which concern moments as they vary with flight con...