GVT-based ground flutter test without wind tunnel

Jie Zeng, Dallas W. Kingsbury, Erich Ritz, Ping Chih Chen, Dong Hwan Lee, Marc Mignolet

Research output: Chapter in Book/Report/Conference proceedingConference contribution

13 Citations (Scopus)

Abstract

A new experimental technique is conceived and validated for the determination of the flutter speed and frequency of vehicles or wings without the need for a wind tunnel. The testing is carried out on the full scale structure subjected to forces, equivalent to the aerodynamic loads, exerted by shakers. The close coupling between the structural response and the aerodynamics is simulated in real time by measuring the response, computing the corresponding aerodynamic forces from a linear state space model, and applying these forces to the structure through the shakers. Besides a significant reduction in cost as compared to wind tunnel testing, the proposed testing strategy also allows for the consideration of structural nonlinearity and the inclusion of flight control system while using the same hardware as would be used in a classic ground vibration test (GVT). The key challenges, successfully resolved here, were the reduction of the distributed aerodynamic loaded to a few concentrated forces and the control of the shakers to provide the necessary force. The technique is demonstrated on a rectangular plate with three different mass distributions and a very good agreement of the observed flutter speeds and frequencies with their counterparts computed from an updated finite element model is obtained.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
DOIs
StatePublished - 2011
Event52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Denver, CO, United States
Duration: Apr 4 2011Apr 7 2011

Other

Other52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
CountryUnited States
CityDenver, CO
Period4/4/114/7/11

Fingerprint

Flutter (aerodynamics)
Wind tunnels
Aerodynamics
Testing
Aerodynamic loads
Flight control systems
Control nonlinearities
Hardware
Costs

ASJC Scopus subject areas

  • Mechanics of Materials
  • Mechanical Engineering
  • Materials Science(all)
  • Aerospace Engineering
  • Architecture

Cite this

Zeng, J., Kingsbury, D. W., Ritz, E., Chen, P. C., Lee, D. H., & Mignolet, M. (2011). GVT-based ground flutter test without wind tunnel. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference [AIAA 2011-1942] https://doi.org/10.2514/6.2011-1942

GVT-based ground flutter test without wind tunnel. / Zeng, Jie; Kingsbury, Dallas W.; Ritz, Erich; Chen, Ping Chih; Lee, Dong Hwan; Mignolet, Marc.

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2011. AIAA 2011-1942.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Zeng, J, Kingsbury, DW, Ritz, E, Chen, PC, Lee, DH & Mignolet, M 2011, GVT-based ground flutter test without wind tunnel. in Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference., AIAA 2011-1942, 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, CO, United States, 4/4/11. https://doi.org/10.2514/6.2011-1942
Zeng J, Kingsbury DW, Ritz E, Chen PC, Lee DH, Mignolet M. GVT-based ground flutter test without wind tunnel. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2011. AIAA 2011-1942 https://doi.org/10.2514/6.2011-1942
Zeng, Jie ; Kingsbury, Dallas W. ; Ritz, Erich ; Chen, Ping Chih ; Lee, Dong Hwan ; Mignolet, Marc. / GVT-based ground flutter test without wind tunnel. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 2011.
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