Add to ORKGThe procedures used to establish the mass matrices characteristics for the fighter type wings studied are given. A description of the procedure used to find the mass associated with a specific aerodynamic panel is presented and some examples of the application of the procedure are included
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
The computer program used to determine the rigid and elastic stability derivatives presented in the ...
An explanation is presented of the method used to locate the elastic axis and the method to determin...
The method used in computing the structural influence coefficient matrix of the computer program of ...
Expressions are derived for computing the aerodynamic influence coefficient matrix for nonplanar win...
Summarized are the aerodynamic center, alpha and q- aeroelastic effects on fighter-type aircraft in ...
In the conceptual aircraft design phase, prediction of the empty weight typically relies on empirica...
Stability derivatives for predicting stability characteristics of elastic aircraf
This note presents the results of flight pressure distribution tests on the right upper wing panel o...
State-of-the-art models in preliminary wing design apply physics-based methods for primary structure...
Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect rat...
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76882/1/AIAA-46232-142.pd
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
The computer program used to determine the rigid and elastic stability derivatives presented in the ...
An explanation is presented of the method used to locate the elastic axis and the method to determin...
The method used in computing the structural influence coefficient matrix of the computer program of ...
Expressions are derived for computing the aerodynamic influence coefficient matrix for nonplanar win...
Summarized are the aerodynamic center, alpha and q- aeroelastic effects on fighter-type aircraft in ...
In the conceptual aircraft design phase, prediction of the empty weight typically relies on empirica...
Stability derivatives for predicting stability characteristics of elastic aircraf
This note presents the results of flight pressure distribution tests on the right upper wing panel o...
State-of-the-art models in preliminary wing design apply physics-based methods for primary structure...
Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect rat...
A formula is derived to calculate structural wing mass. This formula can be applied to twin fuselage...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76882/1/AIAA-46232-142.pd
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76666/1/AIAA-46261-468.pd
The computer program used to determine the rigid and elastic stability derivatives presented in the ...