Christophe AIRIAU
Full professor,
Toulouse III university, France
Department of Mechanics
Institut de Mécanique des Fluides de Toulouse (IMFT)
Research group : Aerodynamics, wakes, interactions (ASI)
9
Documents
Présentation
**Research activities:**
**Teaching activities**
Domaines de recherche
Mécanique des fluides [physics.class-ph]
Mécanique [physics.med-ph]
Compétences
Publications
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Stability and dynamics of the flow past a bullet-shaped blunt body moving in a pipeJournal of Fluid Mechanics, 2022, 948, pp.A18. ⟨10.1017/jfm.2022.564⟩
Article dans une revue
hal-03877593v1
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Adjoint computations by algorithmic differentiation of a parallel solver for time-dependent PDEsJournal of computational science, 2020, 45, pp.101155. ⟨10.1016/j.jocs.2020.101155⟩
Article dans une revue
hal-03033123v1
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Unsteady adjoint computations by algorithmic differentiation of parallel codeJournal of computational science, inPress
Article dans une revue
hal-02865501v1
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On the influence of uncertainty in computational simulations of a high-speed jet flow from an aircraft exhaustComputers and Fluids, 2018, pp.1-20. ⟨10.1016/j.compfluid.2018.12.003⟩
Article dans une revue
hal-01999518v1
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Broadband Shock-cell Noise Signature Identification Using a Wavelet-based Method22nd AIAA/CEAS Aeroacoustics Conference, May 2016, Lyon, France. pp.0, ⟨10.2514/6.2016-2732⟩
Communication dans un congrès
hal-04109368v1
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Adjoint-based acoustic wave sensitivity of a double-stream jetEuromech Colloquium 571, Sep 2016, Palaiseau (France), France
Communication dans un congrès
hal-04429299v1
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A bypass transition in the Lamb-Oseen vortex65th Annual Meeting of the American Physical Society's Division of Fluid Dynamics (DFD), Nov 2012, San Diego, United States. pp.0
Communication dans un congrès
hal-04003377v1
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Generation of a Turbulent Boundary Layer Inflow for RANS Simulations15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), May 2009, Miami, United States. pp.0
Communication dans un congrès
hal-04087841v1
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Active flow control of a two-dimensional compressible cavity flow using direct output feedback lawFondation de la Recherche pour l’Aeronautique et l’Espace. 2013
Rapport
hal-04354217v1
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