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Self-excited oscillation properties of the profile NACA0015 in subsonic flow
- 1.0487855 - ÚT 2019 RIV CZ eng C - Conference Paper (international conference)
Zolotarev, Igor - Vlček, Václav - Kozánek, Jan
Self-excited oscillation properties of the profile NACA0015 in subsonic flow.
DYMAMESI 2018 - Proceedings. Prague: Institute of Thermomechanics AS CR, v. v. i., 2018 - (Zolotarev, I.; Pešek, L.; Kozieň, M.), s. 95-98. ISBN 978-80-87012-66-6.
[DYMAMESI 2018 - Dynamics of Machines and Mechanical Systems with Interactions. Prague (CZ), 06.03.2018-07.03.2018]
Grant - others:AV ČR(CZ) StrategieAV21/3
Program: StrategieAV
Institutional support: RVO:61388998
Keywords : airfoil * aeroelasticity * stall flutter * dynamic stall * limit cycle oscillation * self-excited vibration
OECD category: Fluids and plasma physics (including surface physics)
Self-excited oscillations of the profile NACA0015 in subsonic flow were realized in the wind tunnel. The plunge support had the same elasticity for all experiments, the pitch support had seven different elasticity parameters. During our experiments different types of selfexcited vibration (flutter, stall flutter) were observed. Range of Mach numbers was M = 0.08–0.45, corresponding range of Reynolds numbers is Re = (1–5)·105, when the chord length is used as the characteristic dimension of the profile.
Permanent Link: http://hdl.handle.net/11104/0286759
Number of the records: 1