Your Selections

Frulla, Giacomo
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Authors

Publishers

Affiliations

Events

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings

Published 2015-09-15 by SAE International in United States
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

The Influence of Supersonic Stream on the Dependence "Amplitude-Frequency" of Nonlinear Vibrations of Flexible Plate

Published 2013-09-17 by SAE International in United States
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Efficient Procedure for Robust Optimal Design of Aerospace Laminated Structures

Published 2017-09-19 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams

Published 2017-09-19 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems

Published 2017-09-19 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings

SAE International Journal of Aerospace

  • Journal Article
  • 2013-01-2158
Published 2013-09-17 by SAE International in United States
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings

SAE International Journal of Aerospace

  • Journal Article
  • 2011-01-2722
Published 2011-10-18 by SAE International in United States
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

A Possible Adaptive Wing Apparatus for New UAV Configurations

Published 2015-09-15 by SAE International in United States
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Static/Fatigue Structural Behaviour of Damaged Stiffened Composite Plates for UAS Applications

Published 2013-09-17 by SAE International in United States
Annotation ability available