Status of the KTH-NASA wind-tunnel test for acquisition of transonic nonlinear aeroelastic data
2016 (English)In: 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc , 2016Conference paper (Refereed)Text
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.
IdentifiersURN: urn:nbn:se:kth:diva-186769ScopusID: 2-s2.0-84958078507ISBN: 9781624103988OAI: oai:DiVA.org:kth-186769DiVA: diva2:938627
15th Dynamics Specialists Conference, 2016, 4 January 2016 through 8 January 2016
QC 201606172016-06-172016-05-132016-06-17Bibliographically approved