Add to ORKGA method and program called TRANSEP is presented that can be used for the analysis of the flow about a low speed airfoil under high lift, massive separation conditions. Since the present program is a modification of the direct-inverse TRANDES code, it can also be used for the design and analysis of transonic airfoils, including the effects of weak viscous interaction. Interactions on program usage, program modifications to convert TRANDES to TRANSEP, and sample cases and results are given
Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integ...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
An unstructured-grid, Navier-Stokes flow solver is used to compute the transonic flow development ov...
A direct-inverse technique and computer program called TAMSEP that can be used for the analysis of t...
This report covers the period 1 September 1983 to 31 January 1984. The primary task during this repo...
The input parameters are presented for a computer program which performs calculations for inviscid i...
A computer program was developed to solve the low speed flow around airfoils with highly separated f...
The direct-inverse technique was developed into a numerical method, called TRANDES, that is suitable...
Results are present here for viscous transonic flow over aerofoils to demontrate the capabilities of...
A code developed for simulating high Reynolds number transonic flow fields of arbitrary configuratio...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
The viscous, transonic flow development around the SKF 1.1 supercritical aerofoil section, in clean ...
Navier-Stokes transonic airfoil calculations based on a recently developed nonequilibrium, turbulenc...
A full Navier-Stokes solver has been used to model transonic flow over three airfoil sections. The m...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integ...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
An unstructured-grid, Navier-Stokes flow solver is used to compute the transonic flow development ov...
A direct-inverse technique and computer program called TAMSEP that can be used for the analysis of t...
This report covers the period 1 September 1983 to 31 January 1984. The primary task during this repo...
The input parameters are presented for a computer program which performs calculations for inviscid i...
A computer program was developed to solve the low speed flow around airfoils with highly separated f...
The direct-inverse technique was developed into a numerical method, called TRANDES, that is suitable...
Results are present here for viscous transonic flow over aerofoils to demontrate the capabilities of...
A code developed for simulating high Reynolds number transonic flow fields of arbitrary configuratio...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
The viscous, transonic flow development around the SKF 1.1 supercritical aerofoil section, in clean ...
Navier-Stokes transonic airfoil calculations based on a recently developed nonequilibrium, turbulenc...
A full Navier-Stokes solver has been used to model transonic flow over three airfoil sections. The m...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integ...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
An unstructured-grid, Navier-Stokes flow solver is used to compute the transonic flow development ov...