TY - GEN
T1 - Resolvent analysis of compressible flows over a long rectangular cavity
AU - Liu, Qiong
AU - Sun, Yiyang
AU - Cattafesta, Louis N.
AU - Ukeiley, Lawrence S.
AU - Taira, Kunihiko
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - We perform global instability and resolvent analyses on compressible flows over a long rectangular cavity with a length-to-depth ratio of 6 at a depth-based Reynolds number of 502. The resolvent operator is constructed using the linearized Navier–Stokes equation to analyze the flow response to harmonic forcing. Subsonic and supersonic flows with freestream Mach numbers of 0.6 and 1.4 are studied, respectively. The result indicates that a significant energy amplification arises when the harmonic forcing has a particular combination of frequency and spanwise wavenumber. Later, we introduce unsteady blowing and suction along the cavity leading edge guided by the insights of the resolvent analysis. The unsteady forcing input is a function of spanwise wavenumber and frequency. The spatial structures of the response modes and energy amplifications are well revealed in the 2D controlled flowfields. Moreover, in the 3D case, a prominent decrease of pressure fluctuation is observed above the cavity due to the alleviation of the flow impingement strength on the cavity aft-wall. The current study shows that the resolvent analysis predicts the flow response to the leading edge forcing in direct numerical simulations.
AB - We perform global instability and resolvent analyses on compressible flows over a long rectangular cavity with a length-to-depth ratio of 6 at a depth-based Reynolds number of 502. The resolvent operator is constructed using the linearized Navier–Stokes equation to analyze the flow response to harmonic forcing. Subsonic and supersonic flows with freestream Mach numbers of 0.6 and 1.4 are studied, respectively. The result indicates that a significant energy amplification arises when the harmonic forcing has a particular combination of frequency and spanwise wavenumber. Later, we introduce unsteady blowing and suction along the cavity leading edge guided by the insights of the resolvent analysis. The unsteady forcing input is a function of spanwise wavenumber and frequency. The spatial structures of the response modes and energy amplifications are well revealed in the 2D controlled flowfields. Moreover, in the 3D case, a prominent decrease of pressure fluctuation is observed above the cavity due to the alleviation of the flow impingement strength on the cavity aft-wall. The current study shows that the resolvent analysis predicts the flow response to the leading edge forcing in direct numerical simulations.
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U2 - 10.2514/6.2018-0588
DO - 10.2514/6.2018-0588
M3 - Conference contribution
AN - SCOPUS:85141581418
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -