A High Order Cut Cell Method for Numerical Simulation of Three Dimensional Hypersonic Boundary-Layer Transition with Finite Surface Roughness

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition ◽

10.2514/6.2010-1450 ◽

2010 ◽

Author(s):

Le Duan ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Surface Roughness ◽

Three Dimensional ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

Cell Method ◽

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A high-order cut-cell method for numerical simulation of hypersonic boundary-layer instability with surface roughness

Journal of Computational Physics ◽

10.1016/j.jcp.2010.06.008 ◽

2010 ◽

Vol 229 (19) ◽

pp. 7207-7237 ◽

Author(s):

Le Duan ◽

Xiaowen Wang ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Surface Roughness ◽

Hypersonic Boundary Layer ◽

Cell Method ◽

Cut Cell ◽

Boundary Layer Instability

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High-Order Finite-Difference Schemes for Numerical Simulation of Hypersonic Boundary-Layer Transition

Journal of Computational Physics ◽

10.1006/jcph.1998.6010 ◽

1998 ◽

Vol 144 (2) ◽

pp. 662-709 ◽

Author(s):

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Finite Difference ◽

Difference Schemes ◽

Boundary Layer Transition ◽

Finite Difference Schemes ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

High Order Finite Difference

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Three-dimensional Boundary-Layer Transition Phenomena Investigated by Spatial Direct Numerical Simulation

Laminar-Turbulent Transition ◽

10.1007/978-3-662-03997-7_96 ◽

2000 ◽

pp. 619-624 ◽

Author(s):

Giuseppe Bonfigli ◽

Markus Kloker

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Direct Numerical Simulation ◽

Three Dimensional ◽

Boundary Layer Transition ◽

Layer Transition ◽

Dimensional Boundary

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Harmonic linearized Navier-Stokes equation on describing the effect of surface roughness on hypersonic boundary-layer transition

Physics of Fluids ◽

10.1063/1.5086912 ◽

2019 ◽

Vol 31 (3) ◽

pp. 034108 ◽

Keyword(s):

Boundary Layer ◽

Surface Roughness ◽

Stokes Equation ◽

Boundary Layer Transition ◽

Navier Stokes ◽

Hypersonic Boundary Layer ◽

Navier Stokes Equation ◽

Layer Transition ◽

Effect Of Surface

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Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges. I - A new numerical method and validation

10.2514/6.1997-755 ◽

1997 ◽

Author(s):

Xiaolin Zhong ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Direct Numerical Simulation ◽

Numerical Method ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

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Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack

Physics of Fluids ◽

10.1063/1.3313933 ◽

2010 ◽

Vol 22 (2) ◽

pp. 025105 ◽

Author(s):

Xinliang Li ◽

Dexun Fu ◽

Yanwen Ma

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Direct Numerical Simulation ◽

Small Angle ◽

Angle Of Attack ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition

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Direct Numerical Simulation of Hypersonic Boundary Layer Transition over a Blunt Cone

AIAA Journal ◽

10.2514/1.37305 ◽

2008 ◽

Vol 46 (11) ◽

pp. 2899-2913 ◽

Author(s):

Xinliang Li ◽

Dexun Fu ◽

Yanwen Ma

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Direct Numerical Simulation ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition

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A High Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Arbitrary Surface Roughness

47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ◽

10.2514/6.2009-1337 ◽

2009 ◽

Author(s):

Le Duan ◽

Xiaowen Wang ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Surface Roughness ◽

Cell Method ◽

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Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges. II - Receptivity to sound

10.2514/6.1997-756 ◽

1997 ◽

Author(s):

Xiaolin Zhong ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Direct Numerical Simulation ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

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A High Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Surface Roughness

38th Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2008-3732 ◽

2008 ◽

Author(s):

Le Duan ◽

Xiaowen Wang ◽

Xiaolin Zhong

Keyword(s):

Numerical Simulation ◽

Surface Roughness ◽

Cell Method ◽

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