Add to ORKGInvestigations of the external aerodynamics of the unpowered X-57 using computational fluid dynamics are presented
The role of Computational Fluid Dynamics (CFD) at Ames Research Center has expanded to address a bro...
Wind tunnel tests of a 5.75 scale model of the Boeing Hybrid Wing Body (HWB) configuration were cond...
The NASA Constellation program has relied heavily on Computational Fluid Dynamics simulations for ge...
Investigations of the external aerodynamics of the unpowered X-57 Mod-III configuration using comput...
A computational study of the wing for the distributed electric propulsion X-57 Maxwell airplane conf...
A computational study of the wing for the distributed electric propulsion X-57 Maxwell airplane conf...
Outline - Introduction: X-57 CFD task overview; Motivation. Part I, Computational simulations withou...
The X-57 Maxwell is NASAs latest electric airplane concept that has been simulated for aerodynamic p...
A computational and design study on an airfoil and high-lift flap for the X-57 Maxwell Distributed E...
Reynolds Averaged Navier-Stokes (RANS) simulations were performed on the Lockheed Martin Quiet Super...
An efficient and accurate transonic unsteady aerodynamic method is needed for predicting flight load...
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Re...
Additional developments and enhancements to the XTRAN3S computer program, a code for calculation of ...
NASA's X-57 "Maxwell" flight demonstrator incorporates distributed electric propulsion technologies ...
This study supports the NASA Langley sponsored project aimed at determining the viability of using E...
The role of Computational Fluid Dynamics (CFD) at Ames Research Center has expanded to address a bro...
Wind tunnel tests of a 5.75 scale model of the Boeing Hybrid Wing Body (HWB) configuration were cond...
The NASA Constellation program has relied heavily on Computational Fluid Dynamics simulations for ge...
Investigations of the external aerodynamics of the unpowered X-57 Mod-III configuration using comput...
A computational study of the wing for the distributed electric propulsion X-57 Maxwell airplane conf...
A computational study of the wing for the distributed electric propulsion X-57 Maxwell airplane conf...
Outline - Introduction: X-57 CFD task overview; Motivation. Part I, Computational simulations withou...
The X-57 Maxwell is NASAs latest electric airplane concept that has been simulated for aerodynamic p...
A computational and design study on an airfoil and high-lift flap for the X-57 Maxwell Distributed E...
Reynolds Averaged Navier-Stokes (RANS) simulations were performed on the Lockheed Martin Quiet Super...
An efficient and accurate transonic unsteady aerodynamic method is needed for predicting flight load...
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Re...
Additional developments and enhancements to the XTRAN3S computer program, a code for calculation of ...
NASA's X-57 "Maxwell" flight demonstrator incorporates distributed electric propulsion technologies ...
This study supports the NASA Langley sponsored project aimed at determining the viability of using E...
The role of Computational Fluid Dynamics (CFD) at Ames Research Center has expanded to address a bro...
Wind tunnel tests of a 5.75 scale model of the Boeing Hybrid Wing Body (HWB) configuration were cond...
The NASA Constellation program has relied heavily on Computational Fluid Dynamics simulations for ge...