Add to ORKGAn overview of NASA's Commercial Supersonic Technology (CST) Aeroservoelasticity (ASE) element is provided with a focus on recent computational aeroelastic analyses of a low-boom supersonic configuration developed by Lockheed-Martin and referred to as the N+2 configuration. The overview includes details of the computational models developed to date including a linear finite element model (FEM), linear unsteady aerodynamic models, unstructured CFD grids, and CFD-based aeroelastic analyses. In addition, a summary of the work involving the development of aeroelastic reduced-order models (ROMs) and the development of an aero-propulso-servo-elastic (APSE) model is provided
The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed...
Analytical methods are described for the prediction of aerothermoelastic stability of hypersonic air...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
An overview of recent progress regarding the computational aeroelastic and aeroservoelastic (ASE) an...
A summary of NASA's High Speed Aeroservoelasticity (ASE) project is provided with a focus on a low-b...
A summary of computational and experimental aeroelastic and aeroservoelastic (ASE) results for the S...
A summary of the propulsion system modeling under NASA's High Speed Project (HSP) AeroPropulsoServoE...
A presentation provided at the Fourth National Aerospace Plane Technology Symposium held in Monterey...
Accomplishments and current research projects along four main thrusts in aeroservoelasticity at the ...
This report reviews aeroelastic analyses for propulsion components (propfans, compressors and turbin...
This paper covers the development of an aero-propulso-servo-elastic (APSE) model using computational...
This paper presents details of a flutter and stability analysis of aerospace structures such as hype...
The National Aero-Space Plane (NASP), or X-30, is a single-stage-to-orbit vehicle that is designed t...
To present a summary of frequency domain and time domain procedures for aeroelasticity by using non-...
A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in ...
The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed...
Analytical methods are described for the prediction of aerothermoelastic stability of hypersonic air...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
An overview of recent progress regarding the computational aeroelastic and aeroservoelastic (ASE) an...
A summary of NASA's High Speed Aeroservoelasticity (ASE) project is provided with a focus on a low-b...
A summary of computational and experimental aeroelastic and aeroservoelastic (ASE) results for the S...
A summary of the propulsion system modeling under NASA's High Speed Project (HSP) AeroPropulsoServoE...
A presentation provided at the Fourth National Aerospace Plane Technology Symposium held in Monterey...
Accomplishments and current research projects along four main thrusts in aeroservoelasticity at the ...
This report reviews aeroelastic analyses for propulsion components (propfans, compressors and turbin...
This paper covers the development of an aero-propulso-servo-elastic (APSE) model using computational...
This paper presents details of a flutter and stability analysis of aerospace structures such as hype...
The National Aero-Space Plane (NASP), or X-30, is a single-stage-to-orbit vehicle that is designed t...
To present a summary of frequency domain and time domain procedures for aeroelasticity by using non-...
A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in ...
The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed...
Analytical methods are described for the prediction of aerothermoelastic stability of hypersonic air...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...