Add to ORKGAn airfoil design program and a boundary layer analysis were developed. Boundary conditions were derived for ventilated transonic wind tunnels and performing transonic windtunnel wall calculations. A computational procedure for rotational transonic flow in engine inlet throats was formulated. Results and conclusions are summarized
A numerical investigation of the interaction between a wind tunnel sidewall boundary layer and a thi...
Major emphasis was on the design of shock free airfoils with applications to general aviation. Unste...
Results from the Viscous Transonic Airfoil Workshop are compared with each other and with experiment...
The results are reported of the research on the viscous interactions effects on transonic airfoil de...
Papers presented at the Transonic Symposium are compiled. The following subject areas are covered: N...
Two research programs are described which directly relate to the application of natural laminar flow...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
A theoretical examination of the slotted-wall flow field is conducted to determine the appropriate w...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
An analytical procedure is discussed for designing wall shapes for streamlined, nonporous, two-dimen...
The use of a transonic airfoil code for analysis, inverse design, and direct optimization of an airf...
This report discusses progress made on NASA Cooperative Agreement NCC2-545, 'An Experimental Study o...
A state-of-the-art finite difference boundary-layer program incorporated into the NYU Transonic Anal...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
A numerical investigation of the interaction between a wind tunnel sidewall boundary layer and a thi...
Major emphasis was on the design of shock free airfoils with applications to general aviation. Unste...
Results from the Viscous Transonic Airfoil Workshop are compared with each other and with experiment...
The results are reported of the research on the viscous interactions effects on transonic airfoil de...
Papers presented at the Transonic Symposium are compiled. The following subject areas are covered: N...
Two research programs are described which directly relate to the application of natural laminar flow...
The design of shockless airfoils that are appropriate for experimental work on a supersonic transpor...
An attempt is made to indicate and briefly discuss only the most significant achievements of the res...
A theoretical examination of the slotted-wall flow field is conducted to determine the appropriate w...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
An analytical procedure is discussed for designing wall shapes for streamlined, nonporous, two-dimen...
The use of a transonic airfoil code for analysis, inverse design, and direct optimization of an airf...
This report discusses progress made on NASA Cooperative Agreement NCC2-545, 'An Experimental Study o...
A state-of-the-art finite difference boundary-layer program incorporated into the NYU Transonic Anal...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
A numerical investigation of the interaction between a wind tunnel sidewall boundary layer and a thi...
Major emphasis was on the design of shock free airfoils with applications to general aviation. Unste...
Results from the Viscous Transonic Airfoil Workshop are compared with each other and with experiment...