Validation of a finite element analysis of a flapping wing against inertial and aeroelastic responses

Authors

• Justin K. Mason, Air Force Institute of Technology
• Alan L. Jennings, Air Force Institute of Technology
• Jonathan T. Black, Air Force Institute of Technology
• Alexander E. Sharp, Virginia Military Institute
• Joyce K. Blandino, Virginia Military Institute
• Jacob S. Lysher, Virginia Military Institute

Document Type

Conference Proceeding

Publication Date

4-8-2013

Comments

Session: MAVs and Flapping Wings II

The full conference paper is available from AIAA via subscription or purchase, using the DOI link below.

DOI

10.2514/6.2013-1708

Source Publication

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Recommended Citation

Mason, J. K., Jennings, A. L., Black, J. T., Sharp, A. E., Blandino, J. K., & Lysher, J. S. (2013, April 8). Validation of a finite element analysis of a flapping wing against inertial and aeroelastic responses. 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. https://doi.org/10.2514/6.2013-1708