Method, developed and coded for digital computation, predicts aerodynamic loading on configurations for which linear theory assumptions are violated. Program is written in FORTRAN 4 for use on CDC-6000 series computers
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The ...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
The expanded capabilities for analysis and design of low speed flap systems afforded by recent modif...
Set of programs computes geometric, mass, aerodynamic, and structural effects on fighter and transpo...
A computational system for estimation of nonlinear aerodynamic characteristics of wings at supersoni...
A Computer Code Has Been Developed To Predict The Drag Characteristics Of Missile Configurations At ...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A description of and users manual are presented for a U.S.A. FORTRAN 4 computer program which evalua...
A survey of research on drag-due-to-lift minimization at supersonic speeds, including a study of the...
A wind-tunnel study was conducted to determine the capability of a method combining linear theory an...
This paper introduces an attempt to enhance the accuracy of panel methods. A low-order panel method ...
This paper describes two computer programs which have been combined to obtain inviscid perfect and r...
An integrated system of computer programs has been developed for the design and analysis of superson...
This paper lays out a comprehensive methodology for computing a low-speed, high-lift polar, without ...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The ...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
The expanded capabilities for analysis and design of low speed flap systems afforded by recent modif...
Set of programs computes geometric, mass, aerodynamic, and structural effects on fighter and transpo...
A computational system for estimation of nonlinear aerodynamic characteristics of wings at supersoni...
A Computer Code Has Been Developed To Predict The Drag Characteristics Of Missile Configurations At ...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A description of and users manual are presented for a U.S.A. FORTRAN 4 computer program which evalua...
A survey of research on drag-due-to-lift minimization at supersonic speeds, including a study of the...
A wind-tunnel study was conducted to determine the capability of a method combining linear theory an...
This paper introduces an attempt to enhance the accuracy of panel methods. A low-order panel method ...
This paper describes two computer programs which have been combined to obtain inviscid perfect and r...
An integrated system of computer programs has been developed for the design and analysis of superson...
This paper lays out a comprehensive methodology for computing a low-speed, high-lift polar, without ...
Method permits analysis of noncircular bodies and calculation of wing-body interference effects in p...
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The ...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
The expanded capabilities for analysis and design of low speed flap systems afforded by recent modif...