Add to ORKGThe object of this report is to summarize the work done on 3D transonic flow computations during the year 1986-87. Attempts were made to generate 0 type grids for the fuselage to match with the 0 grids for the wing. In addition a 3D Euler code for wings was developed and applied to several wing configurations ranging from large to moderate aspect ratio. Typical results for a rectangular wing (Aspect ratio of Mv = 0.75 J =2x2019;, as well as cropped delta wing are provided. Comparison with STWING, SFL022 and experiments are made
The solution of time-dependent Euler equations for wings using an explicit Runge-Kutta time-marching...
Some recent experiences with computer programs capable of solving finitie-difference approximations ...
This Note covers attempts to extend an existing two dimensional transonic code, TRADE 1, in Cartesia...
The object of this report is to summarize the work done on 3D transonic flow computations during the...
The object of the present work was to validate the two well known codes STWING and SFL022 to compute...
Three dimensional transonic full potential equation has been solved in conservative and non-conserva...
The transonic full potential code using' body fitted coordinates with ADI/AF2 scheme is under develo...
A simple idea to generate grids for arbitrary shaped finite fuselage with a wing with twist and dihe...
report covers the Phase II progress in a two-phase effort to develop the full-potential finite-volum...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
Three dimensional transonic flow computations are extremely complex due to the nonlinearity in the e...
The use of computational methods for three dimensional transonic flow design and analysis at the Boe...
Euler computations have been made for simulating transonic flow over a cropped Delta wing with a def...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
This report describes a study performed to evaluate a 3D, full potential, computational method devel...
The solution of time-dependent Euler equations for wings using an explicit Runge-Kutta time-marching...
Some recent experiences with computer programs capable of solving finitie-difference approximations ...
This Note covers attempts to extend an existing two dimensional transonic code, TRADE 1, in Cartesia...
The object of this report is to summarize the work done on 3D transonic flow computations during the...
The object of the present work was to validate the two well known codes STWING and SFL022 to compute...
Three dimensional transonic full potential equation has been solved in conservative and non-conserva...
The transonic full potential code using' body fitted coordinates with ADI/AF2 scheme is under develo...
A simple idea to generate grids for arbitrary shaped finite fuselage with a wing with twist and dihe...
report covers the Phase II progress in a two-phase effort to develop the full-potential finite-volum...
A simple- approach has been developed to use the two13; dimensional grid generation method by solvin...
Three dimensional transonic flow computations are extremely complex due to the nonlinearity in the e...
The use of computational methods for three dimensional transonic flow design and analysis at the Boe...
Euler computations have been made for simulating transonic flow over a cropped Delta wing with a def...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
This report describes a study performed to evaluate a 3D, full potential, computational method devel...
The solution of time-dependent Euler equations for wings using an explicit Runge-Kutta time-marching...
Some recent experiences with computer programs capable of solving finitie-difference approximations ...
This Note covers attempts to extend an existing two dimensional transonic code, TRADE 1, in Cartesia...