1–20 von 28 Ergebnissen
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    Optimum Design of Compound Helicopters that Use Higher Harmonic Control

    Giovanetti, Eli B. / Hall, Kenneth C. | AIAA | 2015

    Using Automatic Differentiation to Create a Nonlinear Reduced-Order-Model Aerodynamic Solver

    Thomas, Jeffrey P. / Dowell, Earl H. / Hall, Kenneth C. | AIAA | 2010

    Linearized Euler predictions of unsteady aerodynamic loads in cascades

    HALL, KENNETH C. / CLARK, WILLIAM S. | AIAA | 1993

    Gust response analysis for cascades operating in nonuniform mean flows

    HALL, KENNETH C. / VERDON, JOSEPH M. | AIAA | 1991

    Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities

    Thomas, Jeffrey P. / Hall, Kenneth C. / Dowell, Earl H. | Tema Archiv | 2005

    Sensitivity analysis of the aeroacoustic response of turbomachinery blade rows

    Lorence, Christopher B. / Hall, Kenneth C. | AIAA | 1996

    Stabilization of Explicit Flow Solvers Using a Proper-Orthogonal-Decomposition Technique

    Ekici, Kivanc / Hall, Kenneth C. / Huang, Huang et al. | AIAA | 2013

    Sensitivity analysis of unsteady aerodynamic loads in cascades

    Lorence, Christopher B. / Hall, Kenneth C. | AIAA | 1995

    Gust response analysis for cascades operating in nonuniform mean flows

    Hall, Kenneth C. / Verdon, Joseph M. | NTRS | 1991

    Linearized Euler predictions of unsteady aerodynamic loads in cascades

    Hall, Kenneth C. / Clark, William S. | NTRS | 1993