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    Experimental investigation of the asymmetric body vortex wake

    OBERKAMPF, W. / SHIVANANDA, T. | AIAA | 1980

    Aerodynamics of finned missiles at high angle of attack

    NICOLAIDES, J. / OBERKAMPF, W. | AIAA | 1971

    Drag of bodies of revolution in cavitating flow

    OBERKAMPF, W. / WOLFE, W. | AIAA | 1986

    ESTIMATION OF UNCERTAINTIES FOR A SUPERSONIC RETRO-PROPULSION MODEL VALIDATION EXPERIMENT IN A WIND TUNNEL

    Rhode, M. / Oberkampf, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    A COMPLETE FRAMEWORK FOR VERIFICATION, VALIDATION, AND UNCERTAINTY QUANTIFICATION IN SCIENTIFIC COMPUTING

    Roy, C. / Oberkampf, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Evaluation of boundary-layer and parabolized Navier-Stokes solutionsfor re-entry vehicles

    MCWHERTER, M. / NOACK, R. W. / OBERKAMPF, W. L. | AIAA | 1986

    Flight trajectory simulation of fluid payload projectiles

    VAUGHN, H. / WOLFE, W. / OBERKAMPF, W. | AIAA | 1985

    Flight measurements of a wing tip vortex

    PANTON, R. / OBERKAMPF, W. / SOSKIC, N. | AIAA | 1980

    A New Methodology for the Estimation of Total Uncertainty in Computational Simulation

    Oberkampf, W. / DeLand, S. / Rutherford, B. et al. | British Library Conference Proceedings | 1999

    Surface pressure measurements on a hypersonic vehicle

    Oberkampf, W. / Aeschliman, D. / Henfling, J. et al. | AIAA | 1996

    Flight trajectory simulation of fluid payload projectiles

    VAUGHN, H. R. / WOLFE, W. P. / OBERKAMPF, W. L. | AIAA | 1986