Add to ORKGThe input data required to execute the computer program AIC/INT (aerodynamic influence coefficients with interference) are presented. The purpose of the computer program is to generate aerodynamic forces for a pair of plane and interfering nearly parallel, non-coplanar wings at supersonic Mach numbers. A finite element technique has been employed. Planforms are described by triangular elements and diaphragm regions are generated automatically
A digital computer program has been developed to calculate unsteady loadings caused by motions of li...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
A generalized solution of the hyperbolic wave equation was further developed to relate the velocity ...
The analytical development of unsteady supersonic aerodynamic influence coefficients for isolated an...
The program ISCON (Interacting Supersonic Configuration) is described. The program is in support of ...
The input data required to execute the computer program ISCON are described. The program generates a...
The objective of this research is to develop computationally efficient methods for solving aeroelast...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
Numerical method for evaluation and utilization of supersonic nacelle-wing interferenc
A computer program has been developed to account approximately for the effects of finite wing thickn...
Expressions for calculation of subsonic and supersonic, steady and unsteady aerodynamic forces are d...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
Numerical methods for the design and analysis of arbitrary-planform wings at supersonic speeds are r...
Analytical formulation of the integrated potential approach for general unsteady supersonic configur...
A procedure for computing the aeroelasticity of wings on parallel multiple-instruction, multiple-dat...
A digital computer program has been developed to calculate unsteady loadings caused by motions of li...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
A generalized solution of the hyperbolic wave equation was further developed to relate the velocity ...
The analytical development of unsteady supersonic aerodynamic influence coefficients for isolated an...
The program ISCON (Interacting Supersonic Configuration) is described. The program is in support of ...
The input data required to execute the computer program ISCON are described. The program generates a...
The objective of this research is to develop computationally efficient methods for solving aeroelast...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
Numerical method for evaluation and utilization of supersonic nacelle-wing interferenc
A computer program has been developed to account approximately for the effects of finite wing thickn...
Expressions for calculation of subsonic and supersonic, steady and unsteady aerodynamic forces are d...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
Numerical methods for the design and analysis of arbitrary-planform wings at supersonic speeds are r...
Analytical formulation of the integrated potential approach for general unsteady supersonic configur...
A procedure for computing the aeroelasticity of wings on parallel multiple-instruction, multiple-dat...
A digital computer program has been developed to calculate unsteady loadings caused by motions of li...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
A generalized solution of the hyperbolic wave equation was further developed to relate the velocity ...