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    Structure of supersonic turbulent flow past a sharp fin

    KNIGHT, DOYLE D. / HORSTMAN, C. C. / BOGDONOFF, SEYMOUR et al. | AIAA | 1987

    Developing the Truck Engine for Ultra Low Emissions

    Needham, J R / Faulkner, S A / Doyle, D M | SAGE Publications | 1991

    Structure of supersonic turbulent flow past a swept compression corner

    KNIGHT, DOYLE D. / HORSTMAN, C. C. / BOGDONOFF, SEYMOUR | AIAA | 1992

    Quasiconical Flowfield Structure of the Three-Dimensional Single Fin Interaction

    Doyle D. Knight / Dias Badekast / C . C . Horstmant et al. | AIAA | 1992

    Asymmetric Crossing-Shock-Wave/Turbulent-Boundary-Layer Interaction

    Doyle D. Knight / T. J. Garrison / G. S. Settlest et al. | AIAA | 1995

    Automated Design Optimization for the P2 and P8 Hypersonic Inlets

    Vijay Shukla / Andrew Gelsey / Mark Schwabacher et al. | AIAA | 1997

    Automated Design of a Three-Dimensional Subsonic Diffuser

    Wei-Li Zhang / Doyle D. Knight / Don Smith | AIAA | 2000

    Insights in Turbulence Modeling for Crossing-Shock-Wave/Boundary-Layer Interactions

    Fré, dé / ric Thivet / Doyle D. Knight et al. | AIAA | 2001

    Influence of the Wall Condition on k-? Turbulence Model Predictions

    Fré, dé / ric Thivet / Mirna Daouk et al. | AIAA | 2002

    Plasma Jet for Flight Control

    Anderson, Kellie V. / Knight, Doyle D. | AIAA | 2012

    Thermo-optical vacuum testing of Galileo In-Orbit Validation laser retroreflectors

    Dell’Agnello, S. / Boni, A. / Cantone, C. et al. | Elsevier | 2016

      Thermo-optical vacuum testing of Galileo In-Orbit Validation laser retroreflectors

      Dell’Agnello, S | Online Contents | 2016
      Beteiligte: Doyle, D