Publication date
January 2012
DOI Publisher
American Institute of Aeronautics and Astronautics (AIAA) Language
English Citation count (estimate)
8Abstract
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97067/1/AIAA2012-1758.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97067/1/AIAA2012-1758.pd
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
This paper considers the aeroelastic optimization of a subsonic transport wingbox under a variety of...
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
The optimal shape of flying wings for subsonic and transonic speeds is examined using high-fidelity ...
The optimal shape of flying wings for subsonic and transonic speeds is examined using a suite of too...
A set of techniques is developed that allows the incorporation of flight dynamics metrics as an add...
A set of techniques is developed that allows the incorporation of flight dynamics metrics as an add...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83548/1/AIAA-2010-9199-690.pd
Several minimum-mass optimization problems are solved to evaluate the effectiveness of a variety of ...
The second-generation of supersonic civil transport has to match ambitious targets in terms of noise...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
Over the past decade, growing attention was given to exploring the benefits of engaging numerical mu...
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
This paper considers the aeroelastic optimization of a subsonic transport wingbox under a variety of...
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
The optimal shape of flying wings for subsonic and transonic speeds is examined using high-fidelity ...
The optimal shape of flying wings for subsonic and transonic speeds is examined using a suite of too...
A set of techniques is developed that allows the incorporation of flight dynamics metrics as an add...
A set of techniques is developed that allows the incorporation of flight dynamics metrics as an add...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83548/1/AIAA-2010-9199-690.pd
Several minimum-mass optimization problems are solved to evaluate the effectiveness of a variety of ...
The second-generation of supersonic civil transport has to match ambitious targets in terms of noise...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
Over the past decade, growing attention was given to exploring the benefits of engaging numerical mu...
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
This paper considers the aeroelastic optimization of a subsonic transport wingbox under a variety of...
Minimum-weight aircraft wing design, with an emphasis on avoiding aeroelastic instability, has been ...
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