Add to ORKGA function integral equation governing the unsteady motion of a supersonic cascade is derived. Various representations of the Kernel function are derived and discussed
Finite difference methods for unsteady transonic flow frequency use simplified equations in which ce...
A time-domain Green's Function Method for unsteady supersonic potential flow around complex aircraft...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The derivation of the integral equation which involves this kernel function, originally performed el...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
An analysis was developed that is capable of predicting the linearized unsteady aerodynamics of real...
Experimental data were obtained to help validate analytical and computational fluid dynamics (CFD) c...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
An unsteady potential flow analysis, which accounts for the effects of blade geometry and steady tur...
There is a need for methods to predict the unsteady air loads associated with flutter of turbomachin...
The method is capable of generating approximations of arbitrary accuracy. It is based on approximati...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
Finite difference methods for unsteady transonic flow frequency use simplified equations in which ce...
A time-domain Green's Function Method for unsteady supersonic potential flow around complex aircraft...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The derivation of the integral equation which involves this kernel function, originally performed el...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
An analysis was developed that is capable of predicting the linearized unsteady aerodynamics of real...
Experimental data were obtained to help validate analytical and computational fluid dynamics (CFD) c...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
An unsteady potential flow analysis, which accounts for the effects of blade geometry and steady tur...
There is a need for methods to predict the unsteady air loads associated with flutter of turbomachin...
The method is capable of generating approximations of arbitrary accuracy. It is based on approximati...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
Finite difference methods for unsteady transonic flow frequency use simplified equations in which ce...
A time-domain Green's Function Method for unsteady supersonic potential flow around complex aircraft...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...