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Status of the KTH-NASA wind-tunnel test for acquisition of transonic nonlinear aeroelastic data
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
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2016 (English)In: 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc , 2016Conference paper (Refereed)Text
Abstract [en]

This paper presents a status report on the collaboration between the Royal Institute of Technology (KTH) in Sweden and the NASA Langley Research Center regarding the design, fabrication, modeling, and testing of a full-span fighter configuration in the Transonic Dynamics Tunnel (TDT). The goal of the test is to acquire transonic limit-cycle- oscillation (LCO) data, including accelerations, strains, and unsteady pressures. Finite element models (FEMs) and aerodynamic models are presented and discussed along with results obtained to date.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics Inc , 2016.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-186769ScopusID: 2-s2.0-84958078507ISBN: 9781624103988OAI: oai:DiVA.org:kth-186769DiVA: diva2:938627
Conference
15th Dynamics Specialists Conference, 2016, 4 January 2016 through 8 January 2016
Note

QC 20160617

Available from: 2016-06-17 Created: 2016-05-13 Last updated: 2016-06-17Bibliographically approved

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Ringertz, Ulf TorbjörnStenfelt, GloriaEller, David
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