Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83577/1/AIAA-2010-2707-714.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83584/1/AIAA-2010-2887-116.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76036/1/AIAA-38845-411.pd
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces e...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90666/1/AIAA-2011-2008-958.pd
Results generated from an aeroelastic model obtained by coupling a nonlinear structural dynamic mode...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140673/1/1.j052596.pd
The development of a nonlinear approximate aeroelastic model suitable for representing the behavior ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76665/1/AIAA-2008-1814-283.pd
Results generated from an aeroelastic model obtained by coupling a nonlinear structural dynamic mode...
Flexible flapping wings have garnered a large amount of attention within the micro aerial vehicle (M...
Flexible flapping wings have garnered a large amount of attention within the micro aerial vehicle (M...
This thesis explores the validity of employing quasi-steady aerodynamic models to predict the force...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76845/1/AIAA-2009-1270-256.pd
Direct Numerical Simulations of the flow around a pair of flapping wings are presented. The wings ar...
Direct Numerical Simulations of the flow around a pair of flapping wings are presented. The wings ar...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83584/1/AIAA-2010-2887-116.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76036/1/AIAA-38845-411.pd
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces e...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90666/1/AIAA-2011-2008-958.pd
Results generated from an aeroelastic model obtained by coupling a nonlinear structural dynamic mode...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140673/1/1.j052596.pd
The development of a nonlinear approximate aeroelastic model suitable for representing the behavior ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76665/1/AIAA-2008-1814-283.pd
Results generated from an aeroelastic model obtained by coupling a nonlinear structural dynamic mode...
Flexible flapping wings have garnered a large amount of attention within the micro aerial vehicle (M...
Flexible flapping wings have garnered a large amount of attention within the micro aerial vehicle (M...
This thesis explores the validity of employing quasi-steady aerodynamic models to predict the force...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76845/1/AIAA-2009-1270-256.pd
Direct Numerical Simulations of the flow around a pair of flapping wings are presented. The wings ar...
Direct Numerical Simulations of the flow around a pair of flapping wings are presented. The wings ar...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83584/1/AIAA-2010-2887-116.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76036/1/AIAA-38845-411.pd
A range of quasi-steady and unsteady aerodynamic models are used to predict the aerodynamic forces e...
DOI
Add to ORKG