Effect of Local Thermal Strips on Hypersonic Boundary-Layer Instability
Tài liệu tham khảo
Johnson, 2005, Hypersonic boundary layer stability analysis using PSE-Chem
Van Driest, 1952, Investigation of laminar boundary layer in compressible fluids using the Crocco method, NACA Tech
Mack L. Boundary-layer linear stability theory. AGARD Rep. 709. 1984, https://apps.dtic.mil/sti/citations/ADP004046.
Masad, 1995, On transition in supersonic and hypersonic boundary layers, International journal of engineering science, 33, 1893, 10.1016/0020-7225(95)00046-Z
Soudakov, 2009, Numerical simulation of receptivity of a hypersonic boundary layer over a surface with temperature jump
Sidorenko, 2015, Effect of the local wall cooling/heating on the hypersonic boundary-layer stability and transition, Progress in Flight Physics, 7, 549, 10.1051/eucass/201507549
Fedorov, 2015, High-speed boundary-layer stability on a cone with localized wall heating or cooling, AIAA J, 53, 2512, 10.2514/1.J053666
Zhao, 2018, Numerical simulation of local wall heating and cooling effect on the stability of a hypersonic boundary layer, International Journal of Heat and Mass Transfer, 121, 986, 10.1016/j.ijheatmasstransfer.2018.01.054
Batista, 2020, Local wall temperature effects on the second-mode instability, Journal of Spacecraft and Rockets, 57, 580, 10.2514/1.A34620
Zhao, 2022, Effect of surface temperature strips on the evolution of supersonic and hypersonic Mack modes: Asymptotic theory and numerical results, Physical Review Fluids, 7, 10.1103/PhysRevFluids.7.053901
Park, 2016, Study of effect of a smooth hump on hypersonic boundary layer instability, Theoretical and Computational Fluid Dynamics, 30, 543, 10.1007/s00162-016-0396-7
Fedorov, 2011, High-speed boundary-layer instability: old terminology and a new framework, AIAA J, 49, 1647, 10.2514/1.J050835
Kendall, 1975, Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition, AIAA J, 13, 290, 10.2514/3.49694
Jaffe, 1970, Determination of spatial amplification factors and their application to predicting transition, AIAA J, 8, 301, 10.2514/3.5660
Johnson, 1998, Numerical study of hypersonic reacting boundary layer transition on cones, Physics of Fluids, 10, 2676, 10.1063/1.869781
Johnson, 2006, Analysis of Laminar-Turbulent Transition in Hypersonic Flight Using PSE-Chem
Fong, 2014, Numerical simulation of roughness effect on the stability of a hypersonic boundary layer, Computers & Fluids, 96, 350, 10.1016/j.compfluid.2014.01.009
Kim, 2019, Large-eddy simulation with parabolized stability equations for turbulent transition using OpenFOAM, Computers & Fluids, 189, 108, 10.1016/j.compfluid.2019.04.010
Lim, 2022, Simulation of hypersonic boundary layer on porous surfaces using OpenFOAM, Computers & Fluids, 240, 10.1016/j.compfluid.2022.105437
Lim J, Kim M, Kim S, Jee S, and Park D. PSE-Coupled LES Method for Turbulent Transition in Compressible Boundary Layer. In: AIAA SCITECH 2022 Forum 2022, 10.2514/6.2022-0476.
Boris, 1990, On large eddy simulation using subgrid turbulence models Comment 1
Lesieur, 1996, New trends in large-eddy simulations of turbulence, Annual review of fluid mechanics, 28, 45, 10.1146/annurev.fl.28.010196.000401
Tufts, 2019, Implicit Large-Eddy Simulation of Discrete Roughness Boundary-Layer Transition with Added Perturbations
Li, 2020, A compressible solver for the laminar-turbulent transition in natural convection with high temperature differences using implicit large eddy simulation, International Communications in Heat and Mass Transfer, 117, 10.1016/j.icheatmasstransfer.2020.104721
Parent, 2018, Positivity-preserving dual time stepping schemes for gas dynamics, Journal of Computational Physics, 361, 391, 10.1016/j.jcp.2018.01.046
Roe, 1981, Approximate Riemann solvers, parameter vectors, and difference schemes, Journal of computational physics, 43, 357, 10.1016/0021-9991(81)90128-5
Anderson, 1986, Comparison of finite volume flux vector splittings for the Euler equations, AIAA J, 24, 1453, 10.2514/3.9465
Balsara, 2016, An efficient class of WENO schemes with adaptive order, Journal of Computational Physics, 326, 780, 10.1016/j.jcp.2016.09.009
Nayfeh, 1988, Effect of bulges on the stability of boundary layers, The Physics of fluids, 31, 796, 10.1063/1.866815
Masad, 1994, Transition prediction and control in subsonic flow over a hump, Physics of Fluids, 6, 313, 10.1063/1.868086
Iyer, 1989, Computation of three-dimensional compressible boundary layers to fourth-order accuracy on wings and fuselages
Ma, 2003, Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions, Journal of Fluid Mechanics, 488, 31, 10.1017/S0022112003004786
Ma, 2003, Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound, Journal of Fluid Mechanics, 488, 79, 10.1017/S0022112003004798
Tumin, 2011, Numerical simulation and theoretical analysis of perturbations in hypersonic boundary layers, AIAA J, 49, 463, 10.2514/1.J050431
Wang, 2009, Effect of wall perturbations on the receptivity of a hypersonic boundary layer, Physics of fluids, 21, 10.1063/1.3103880
Wang, 2011, Response of a hypersonic boundary layer to wall blowing-suction, AIAA J, 49, 1336, 10.2514/1.J050173
Park, 2013, Influence of two-dimensional smooth humps on linear and non-linear instability of a supersonic boundary layer, Computers & Fluids, 79, 140, 10.1016/j.compfluid.2013.03.018
Park, 2013, Linear and non-linear stability analysis of incompressible boundary layer over a two-dimensional hump, Computers & Fluids, 73, 80, 10.1016/j.compfluid.2012.12.007
Fong, 2015, Parametric study on stabilization of hypersonic boundary layer waves using 2-D surface roughness
Egorov, 2006, Direct numerical simulation of disturbances generated by periodic suction-blowing in a hypersonic boundary layer, Theoretical and Computational Fluid Dynamics, 20, 41, 10.1007/s00162-005-0001-y
Wang, 2012, The stabilization of a hypersonic boundary layer using local sections of porous coating, Physics of fluids, 24, 10.1063/1.3694808
Wang, 2008, Role of the synchronization point on boundary layer stabilization using porous coating
Chang, 2021, Wall Cooling Effect on High-Enthalpy Supersonic Modes over a Cone, AIAA J, 59, 3831, 10.2514/1.J060161