1–16 of 16 hits
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    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. / VATSA, V. N. / KINARD, T. A. | AIAA | 1972

    Solution of slightly underexpanded axisymmetric coflowing jets

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

    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

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

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

    Analysis of urban development of Haridwar, India, using entropy approach

    Jha, Ramakar / Singh, Vijay P. / Vatsa, V. | Springer Verlag | 2008

    Analysis of airfoil leading edge separation bubbles

    VATSA, V. / CARTER, J. | AIAA | 1983

    Analysis of airfoil leading-edge separation bubbles

    VATSA, V. N. / UniversityTechnologies Research Center / East Hartford et al. | AIAA | 1984