Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data

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Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data

Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data

Silva, Walter A. / Chwalowski, Pawel / Wieseman, Carol D. / Eller, David / Ringertz, Ulf

A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in Sweden and the NASA Langley Research Center regarding the aeroelastic analyses of a full-span fighter configuration wind-tunnel model. This wind-tunnel model was tested in the Transonic Dynamics Tunnel (TDT) in the summer of 2016. Large amounts of data were acquired including steady/unsteady pressures, accelerations, strains, and measured dynamic deformations. The aeroelastic analyses presented include linear aeroelastic analyses, CFD steady analyses, and analyses using CFD-based reduced-order models (ROMs).

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Title :

Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data

Contributors:

Silva, Walter A. (author) / Chwalowski, Pawel (author) / Wieseman, Carol D. (author) / Eller, David (author) / Ringertz, Ulf (author)

Conference:

SciTech Forum ; 2017 ; Grapevine, TX, United States

Publication date :

2017-01-09

Type of media :

Conference paper

Type of material :

No indication

Language :

English

Keywords :

Aircraft Design, Testing And Performance , Computer Programming And Software

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