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    Viscous/inviscid interaction analysis of separated trailing-edge flows

    VATSA, V. / VERDON, J. | AIAA | 1984

    Viscid/inviscid interaction at laminar and turbulent symmetric trailing edges

    VERDON, J. / VATSA, V. / WERLE, M. | AIAA | 1982

    Viscid/inviscid interaction analysis of separated trailing-edge flows

    Vatsa, V. N. / Verdon, J. M. | NTRS | 1985

    Viscid/inviscid interaction analysis of separated trailing-edge flows

    VATSA, V. N. / United Technologies Research Center / East Hartford et al. | AIAA | 1985

    Transonic Navier-Stokes flow computations over wing-fuselage geometries

    AGRAWAL, S. / KINARD, T. / VATSA, V. | AIAA | 1991

      Transonic Navier-Stokes Flow Computations over Wing-Fuselage Geometries

      Agrawal, S. / Kinard, T. / Vatsa, V. et al. | British Library Conference Proceedings | 1991

    Transonic Navier-Stokes flow computations over wing-fuselage geometries

    Agrawal, S. / Vatsa, V. N. / Kinard, T. A. | NTRS | 1993

    Transonic Navier-Stokes flow computations over wing-fuselage geometries

    AGRAWAL, S. / VATSA, V. N. / KINARD, T. A. | AIAA | 1972

    Solution of slightly underexpanded axisymmetric coflowing jets

    VATSA, V. / WERLE, M. / ANDERSON, O. | AIAA | 1980

    RE-EVALUATION OF AN OPTIMIZED SECOND-ORDER BACKWARD DIFFERENCE (BDF2OPT) SCHEME FOR UNSTEADY FLOW APPLICATIONS

    Vatsa, V. / Carpenter, M. / Lockard, D. et al. | British Library Conference Proceedings | 2010

    Reduced-Order Models for the Aeroelastic Analysis of the Ares Vehicles

    Silva, W. / Vatsa, V. / Biedron, R. et al. | British Library Conference Proceedings | 2010

    Numerical study of separated laminar boundary layers over multiple sine-wave protuberances

    POLAK, A. / WERLE, M. J. / VATSA, V. N. et al. | AIAA | 1976

    Numerical Simulation of a High-Lift Configuration with Embedded Fluidic Actuators (AIAA 2014-2142)

    Vatsa, V. / Casalino, D. / Lin, J. et al. | British Library Conference Proceedings | 2014

    Navier-Stokes solutions for transonic flow over a wing mounted in a tunnel

    VATSA, V. / WEDAN, B. | AIAA | 1988

    Navier-Stokes computations of prolate spheroids at angle of attack

    VATSA, V. / THOMAS, J. / WEDAN, B. | AIAA | 1987

    Inverse design of nacelles using multi-block Navier Stokes codes

    Naik, D / Krist, S / Campbell, R et al. | AIAA | 1995

    Inverse Design of Nacelles Using Multi-Block Navier Stokes Codes

    Naik, D. A. / Krist, S. E. / Campbell, R. L. et al. | NTRS | 1995

    Global artificial boundary conditions for computation of external flows with jets

    Tsynkov, S. / Abarbanel, S. / Nordström, J. et al. | Tema Archive | 2000

    FUN3D Grid Refinement and Adaptation Studies for the Ares Launch Vehicle

    Bartels, R. / Vatsa, V. / Carlson, J. et al. | British Library Conference Proceedings | 2010

    FLUID DYNAMICS - Global Artificial Boundary Conditions for Computation of External Flows with Jets

    Tsynkov, S. | Online Contents | 2000
    Contributors: Vatsa, V.

    Effect of sidewall boundary layer on a wing in a wind tunnel

    VATSA, V. N. / WEDAN, B. W. | AIAA | 1989

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