The transient growth of a counter-rotating equal strength vortex pair, which descends under mutual induction towards a ground plane, is examined through non-modal linear stability analysis and direct numerical simulation. The vortex pair is studied at a height of five vortex spacing distances above the wall, consistent with the first mode of vortex instability/wall interaction observed by experiment. Three regimes are identified in which the optimal mode topology and non-modal growth mechanisms are distinct, correlated with the widely studied Crow and elliptic instabilities, alongside a wall-modified long-wavelength-displacement-type instability. The initial optimal amplification mechanisms are found to be weakly influenced by the wall, with the long- and short-wave mechanisms consisting of anti-symmetric amplification at the leading hyperbolic point and symmetric amplification at the trailing hyperbolic point, respectively, as observed by out-of-wall studies previously. The linear growth of the Crow instability is found to be impeded by the wall, and the evolution results in the suppression of both the secondary structure formation and vortex rebound. The linear elliptic mode remains largely uninhibited however, and substantially outgrows the long-wave modes, illustrating the importance of the elliptic instability on the wall-bounded interaction. Both the wall-modified long-wave and elliptic optimal growth modes show substantial amplification in the secondary vortices. At finite perturbation amplitudes, the nonlinear formation of both long- and short-wavelength secondary vortex tongues are shown to play a critical role in the vortex dynamics as the pair strongly interacts with the wall.
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Univ Nacl Autonoma Mexico, Fac Ciencias, Dept Matemat, Mexico City 04510, DF, MexicoUniv Nacl Autonoma Mexico, Fac Ciencias, Dept Matemat, Mexico City 04510, DF, Mexico
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Macquarie Univ, Dept Engn, N Ryde, NSW 2109, AustraliaUNSW Australia, Sch Mech & Mfg Engn, Sydney, NSW 2052, Australia
Diasinos, Sammy
Doig, Graham
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UNSW Australia, Sch Mech & Mfg Engn, Sydney, NSW 2052, Australia
Calif Polytech State Univ San Luis Obispo, Aerosp Engn Dept, San Luis Obispo, CA 93407 USAUNSW Australia, Sch Mech & Mfg Engn, Sydney, NSW 2052, Australia
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Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, CA 90095-1597, United States
Department of Mechanical Engineering, McGill University, Montreal, Que., CanadaDepartment of Mechanical and Aerospace Engineering, University of California, Los Angeles, CA 90095-1597, United States
Cortelezzi, L.
Karagozian, A.R.
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Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, CA 90095-1597, United StatesDepartment of Mechanical and Aerospace Engineering, University of California, Los Angeles, CA 90095-1597, United States
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Univ Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USAUniv Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USA
Cortelezzi, L
Karagozian, AR
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Univ Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USAUniv Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USA
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China Univ Min & Technol, Sch Sci, Beijing 100083, Peoples R ChinaChina Univ Min & Technol, Sch Sci, Beijing 100083, Peoples R China
Li, Z. L.
Li, Y. J.
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China Univ Min & Technol, Sch Sci, Beijing 100083, Peoples R ChinaChina Univ Min & Technol, Sch Sci, Beijing 100083, Peoples R China
Li, Y. J.
Xie, B. S.
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Beijing Normal Univ, Coll Nucl Sci & Technol, Beijing 100875, Peoples R China
Beijing Radiat Ctr, Beijing 100875, Peoples R ChinaChina Univ Min & Technol, Sch Sci, Beijing 100083, Peoples R China