Add to ORKGThe five basic elements of the two dimensional airfoil research program at Ames Research Center are illustrated. These elements are experimental, theoretical (including computational), validation, design optimization, and industry interaction. Each area is briefly discussed
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
The abilities of two different Reynolds-Averaged Navier-Stokes codes to predict the effects of an ac...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report discusses progress made on NASA Cooperative Agreement NCC2-545, 'An Experimental Study o...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and con...
Full-potential, Euler, and Navier-Stokes computational fluid dynamics (CFD) codes were evaluated for...
Two flight tests have been conducted that obtained extension pressure data on a modified AH-1G rotor...
Papers given at the conference present the results of theoretical research on aerodynamic flow probl...
Recent developments in airfoil-testing methods and fundamental air-flow investigations, as applied t...
Five full scale rotorcraft airfoils were tested in the NASA Ames Eleven-Foot Transonic Wind Tunnel f...
Airfoil plays an important role in any aircraft because it has to generate adequate lift to hold the...
A high-lift workshop was held in May of 1993 at NASA Langley Research Center. A major part of the wo...
The report documents the study of the application of the TRAC airfoil table computational package (T...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
The abilities of two different Reynolds-Averaged Navier-Stokes codes to predict the effects of an ac...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report discusses progress made on NASA Cooperative Agreement NCC2-545, 'An Experimental Study o...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and con...
Full-potential, Euler, and Navier-Stokes computational fluid dynamics (CFD) codes were evaluated for...
Two flight tests have been conducted that obtained extension pressure data on a modified AH-1G rotor...
Papers given at the conference present the results of theoretical research on aerodynamic flow probl...
Recent developments in airfoil-testing methods and fundamental air-flow investigations, as applied t...
Five full scale rotorcraft airfoils were tested in the NASA Ames Eleven-Foot Transonic Wind Tunnel f...
Airfoil plays an important role in any aircraft because it has to generate adequate lift to hold the...
A high-lift workshop was held in May of 1993 at NASA Langley Research Center. A major part of the wo...
The report documents the study of the application of the TRAC airfoil table computational package (T...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
The abilities of two different Reynolds-Averaged Navier-Stokes codes to predict the effects of an ac...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...