Add to ORKGThis presentation presents the analysis of stall behavior of a wing based on Prandtl's work on minimum induced drag
Computational fluid dynamics (CFD) analysis was conducted to study the low-speed stall aerodynamics ...
Improvements in the aerodynamic efficiency of commercial transport aircraft will reduce fuel usage w...
We present LES simulations of the flow over a wing with sinusoidal leading edge undulations. The und...
Stall characteristics of a wing whose design was based on Prandtls minimum induced drag analysis is ...
Stall characteristics of a wing designed based on Prandtls minimum induced drag solution using the b...
In order to fly, an aircraft of a given weight needs to produce an equal but opposite force to this w...
For nearly a century Ludwig Prandtl's lifting-line theory remains a standard tool for understanding ...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
Reynolds-Averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) analysis was conducted: to...
A method is presented for calculating the spanwise lift distribution on straight-wing/propeller comb...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
A computational analysis was performed to address the effects of walls on wings rotating at a Reynol...
This is the presentation related to the paper of the same name describing Reynolds Averaged Navier S...
The present paper is the second part of a combined (experimental and computational) study on stall c...
The results of a parametric wing design study using a modern laminar flow airfoil designed to exhibi...
Computational fluid dynamics (CFD) analysis was conducted to study the low-speed stall aerodynamics ...
Improvements in the aerodynamic efficiency of commercial transport aircraft will reduce fuel usage w...
We present LES simulations of the flow over a wing with sinusoidal leading edge undulations. The und...
Stall characteristics of a wing whose design was based on Prandtls minimum induced drag analysis is ...
Stall characteristics of a wing designed based on Prandtls minimum induced drag solution using the b...
In order to fly, an aircraft of a given weight needs to produce an equal but opposite force to this w...
For nearly a century Ludwig Prandtl's lifting-line theory remains a standard tool for understanding ...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
Reynolds-Averaged Navier-Stokes (RANS) computational fluid dynamics (CFD) analysis was conducted: to...
A method is presented for calculating the spanwise lift distribution on straight-wing/propeller comb...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
A computational analysis was performed to address the effects of walls on wings rotating at a Reynol...
This is the presentation related to the paper of the same name describing Reynolds Averaged Navier S...
The present paper is the second part of a combined (experimental and computational) study on stall c...
The results of a parametric wing design study using a modern laminar flow airfoil designed to exhibi...
Computational fluid dynamics (CFD) analysis was conducted to study the low-speed stall aerodynamics ...
Improvements in the aerodynamic efficiency of commercial transport aircraft will reduce fuel usage w...
We present LES simulations of the flow over a wing with sinusoidal leading edge undulations. The und...