1–24 of 24 hits
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    The use of heavy gas for increased Reynolds numbers in transonic wind tunnels

    Anders, J. / Anderson, W. / Murthy, A. | AIAA | 1998

    Sensitivity analysis for the Navier-Stokes equations on unstructured meshes using complex variables

    Anderson, W. / Newman, James / Whitfield, David et al. | AIAA | 1999

    Analysis and Design of Solid Oxide Fuel Cells with Advanced Numerical Techniques

    Elliott, Louie / Anderson, W. / Kapadia, Sagar et al. | AIAA | 2007

    A multiblock approach for calculating incompressible fluid flows on unstructured grids

    Sheng, Chunhua / Whitfield, David / Anderson, W. | AIAA | 1997

    Numerical analysis concepts for balloon analysis

    Anderson, W. / Park, Jungsun / Dungan, Michael | AIAA | 1994

    Analysis and Experiments of Hydrogen Peroxide Vaporization and Decomposition

    Mok, J. S. / Sisco, J. / Anderson, W. | AIAA | 2003

    Development of a reduced mechanism for the double base propellant dark zone

    Ilincic, N. / Seshadri, K. / Anderson, W. | AIAA | 1996

    Acoustic Mode Simulations in Experimental Rocket Combustors

    Ellis, M. / Xia, Guoping / Sankaran, V. et al. | AIAA | 2005

    An O(Nm2) plane solver for the compressible Navier-Stokes equations

    Thomas, J. / Bonhaus, D. / Anderson, W. et al. | AIAA | 1999

    Propulsion Educational Programs and Facilities at Purdue University

    Heister, Stephen / Meyer, S. / Anderson, W. et al. | AIAA | 2004

    Upper Stage Flight Experiment 10K engine design and test results

    Ross, R. / Morgan, D. / Crockett, D. et al. | AIAA | 2000

    Lorentz force accelerator with an open-ended lithium heat pipe

    Choueiri, E. / Chiravalle, V. / Miller, George et al. | AIAA | 1996

    Catalyst development for hydrogen peroxide rocket engines

    Morlan, P. / Wu, P.-K. / Ruttle, D. et al. | AIAA | 1999

    Development of a pressure-fed rocket engine using hydrogen peroxide and JP-8

    Wu, P.-K. / Fuller, R. / Morlan, P. et al. | AIAA | 1999

    Impinging jet flow structure and its impact on combustion instability

    Santoro, R. / Woodward, R. / Schmidt, J. et al. | AIAA | 1998

    Low cost propulsion using a high density, storable, and clean propellant combination

    Anderson, W. / Crockett, D. / Hill, S. et al. | AIAA | 1998