Add to ORKGThe direct-inverse technique was developed into a numerical method, called TRANDES, that is suitable for the analysis and design of subsonic and transonic airfoils and for the evaluation of design concepts. A general description of the method is given and its application to a design analysis type of problem is demonstrated. A usage of the method for the low speed high lift case is discussed
A low speed airfoil design and analysis program was developed which contains several unique features...
AbstractThe paper presents a computationally efficient and robust methodology for the inverse design...
Some ideas for using hodograph theory, mapping techniques and methods of characteristics to formulat...
A numerical technique for designing transonic airfoils having a prescribed pressure distribution (th...
A direct-inverse technique and computer program called TAMSEP that can be used for the analysis of t...
Aerodynamic characteristics are very sensitive to airfoil leading-edge geometry, and its accurate tr...
The results are reported of the research on the viscous interactions effects on transonic airfoil de...
A direct-inverse approach to the transonic design problem was presented in its initial state at the ...
Several inverse methods were compared and initial results indicate that differences in results are p...
A hybrid inverse/direct-optimization method for subsonic/transonic airfoil and wing shape design is ...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An inverse wing design method was developed around an existing transonic wing analysis code. The ori...
The feasibility of the use of the Navier-Stokes equations in aerodynamic design is examined. The Nav...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
Several inverse methods have been compared and initial results indicate that differences in results ...
A low speed airfoil design and analysis program was developed which contains several unique features...
AbstractThe paper presents a computationally efficient and robust methodology for the inverse design...
Some ideas for using hodograph theory, mapping techniques and methods of characteristics to formulat...
A numerical technique for designing transonic airfoils having a prescribed pressure distribution (th...
A direct-inverse technique and computer program called TAMSEP that can be used for the analysis of t...
Aerodynamic characteristics are very sensitive to airfoil leading-edge geometry, and its accurate tr...
The results are reported of the research on the viscous interactions effects on transonic airfoil de...
A direct-inverse approach to the transonic design problem was presented in its initial state at the ...
Several inverse methods were compared and initial results indicate that differences in results are p...
A hybrid inverse/direct-optimization method for subsonic/transonic airfoil and wing shape design is ...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An inverse wing design method was developed around an existing transonic wing analysis code. The ori...
The feasibility of the use of the Navier-Stokes equations in aerodynamic design is examined. The Nav...
The multiphase effort in the development of tools for the analysis and design of two-element airfoil...
Several inverse methods have been compared and initial results indicate that differences in results ...
A low speed airfoil design and analysis program was developed which contains several unique features...
AbstractThe paper presents a computationally efficient and robust methodology for the inverse design...
Some ideas for using hodograph theory, mapping techniques and methods of characteristics to formulat...