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    A perspective on computational aerothermodynamics: current modelling difficulties

    Candler, G. V. | British Library Online Contents | 1995

    Particle and Continuum Method Comparison of a High-Altitude, Extreme-Mach-Number Reentry Flow

    Ozawa, T. / Levin, D. A. / Nompelis, I. et al. | AIAA | 2010

    Numerical simulation of nonequilibrium condensation in a hypersonic wind tunnel

    Perrell, E. R. / Erickson, W. D. / Candler, G. V. | AIAA | 1996

    Simulation of a Three-Dimensional Flapping Cantilever for Micro Air Vehicle Propulsion

    Emblemsvag, J.-E. / Suzuki, R. / Candler, G. V. et al. | British Library Conference Proceedings | 2003

    Experimental and Numerical Investigation of Hypervelocity Carbon Dioxide Flow over Blunt Bodies

    Sharma, M. / Swantek, A. B. / Flaherty, W. et al. | AIAA | 2010

    Navier-Stokes solutions with surface catalysis for Martian atmospheric entry

    CHEN, Y.-K. / HENLINE, W. D. / STEWART, D.A. et al. | AIAA | 1993

    Computations for support design of measurements of radiation from low velocity shocked air

    LEVIN, D. A. / COLLINS, R. J. / CANDLER, G. V. | AIAA | 1991

    Comparison of coupled radiative flow solutions with Project Fire II flight data

    Olynick, David R. / Henline, W. D. / Chambers, Lin H. et al. | AIAA | 1995

    Computational Analysis of Hypersonic Laminar Viscous-Inviscid Interactions

    Candler, G. V. / Nompelis, I. / Holden, M. S. et al. | British Library Conference Proceedings | 2000

    Numerical Investigations of Supersonic Base Flows Using DES

    Subbareddy, P. / Candler, G. V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005

    Computational Simulation of Laser-Induced Plasmas for Supersonic Flow Control

    Kandala, R. / Candler, G. V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004

    AIAA 2006-0405 Flow Control of Swept Fin Shock Interactions by Laser-Induced Plasmas

    Trumble, K. A. / Candler, G. V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    Detached Eddy Simulation of Supersonic Base Flow with Bleed

    Subbareddy, P. / Candler, G. V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004

    Nonequilibrium Effects on Hypersonic Boundary Layers and Inviscid Stability

    Hudson, M. L. / Chokani, N. / Candler, G. V. et al. | British Library Conference Proceedings | 1994

    Theory of radiation from low velocity shock heated air

    LEVIN, D. A. / LODA, R. T. / CANDLER, G. V. et al. | AIAA | 1993

    Numerical Study of Hypersonic Boundary Layer Transition on a Blunt Body

    Johnson, H. B. / Candler, G. V. / Hudson, M. L. et al. | British Library Conference Proceedings | 1997

    A Data-Parallel LU-SGS Method for Reacting Flows

    Candler, G. V. / Wright, M. J. / McDonald, J. D. et al. | British Library Conference Proceedings | 1994

    Numerical Simulations of Atlas-II Rocket Motor Plumes

    Candler, G. V. / Rao, R. M. / Sinha, K. et al. | British Library Conference Proceedings | 2001

    Hypersonic Inward Turning Inlets: Design and Optimization (AIAA 2006-0297)

    Drayna, T. W. / Nompelis, I. / Candler, G. V. et al. | British Library Conference Proceedings | 2006

    Modeling the Effect of Shock Unsteadiness in Shock-wave / Turbulent Boundary Layer Interactions

    Sinha, K. / Mahesh, K. / Candler, G. V. et al. | British Library Conference Proceedings | 2004

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