1–45 von 45 Ergebnissen
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    The concept of lateral blowing

    TAVELLA, D. / ROBERTS, L. | AIAA | 1985

    Instability of Adverse-Pressure-Gradient Boundary Layers with Suction

    Roberts, P. J. D. / Floryan, J. M. | AIAA | 2008

    The stability of a tethered gyromill

    RYE, D. / ROBERTS, B. | AIAA | 1981

    NuSTAR Ground Systems Approach - Lessons Learned

    Bester, Manfred / Roberts, Bryce / Lewis, Mark D. et al. | AIAA | 2013

    Structural Analysis of the Redesigned Ice/Frost Ramp Bracket

    Phillips, D / Dawicke, D / Gentz, S et al. | AIAA | 2007

    On the Initial Characterization of a Large-Scale Hypervelocity Expansion Tunnel

    Dean, Tyler / Blair, Trevor R. / Roberts, McKenna et al. | AIAA | 2022

    Compressibility Effects on Boundary-Layer Transition Induced by an Isolated Roughness Element

    Redford, John A. / Sandham, Neil D. / Roberts, Graham T. | AIAA | 2010

    Analysis of interacting dual lifting ejector systems

    LUND, T. / TAVELLA, D. / ROBERTS, L. | AIAA | 1986

    A zonal computational approach to thrust augmentor optimization

    LUND, T. / TAVELLA, D. / ROBERTS, L. | AIAA | 1985

    Flow structure of lateral wing-tip blowing

    LEE, C. / TAVELLA, D. / WOOD, N. et al. | AIAA | 1986

    Flow structure and scaling laws in lateral wing-tip blowing

    LEE, C. S. / TAVELLA, D. / WOOD, N. J. et al. | AIAA | 1989

    Rocket exhaust plume induced flowfield interaction experiences with the Space Shuttle

    ROBERTS, B. / WALLACE, R. / CRAIG, M. et al. | AIAA | 1983

    An investigation of film cooling on a hypersonic vehicle using a PNSflow analysis code

    BANKEN, G. / ROBERTS, D. / HOLCOMB, J. et al. | AIAA | 1985

    The jet spoiler as a yaw control device

    TAVELLA, D. / LEE, C. / WOOD, N. et al. | AIAA | 1986

    Thrust augmentor inlet optimization

    LUND, T. S. / TAVELLA, D. A. / ROBERTS, L. | AIAA | 1986

    Lift modulation with lateral wing-tip blowing

    TAVELLA, D. A. / WOOD, N. J. / LEE, C. S. et al. | AIAA | 1988

    Engine thrust measurement uncertainty

    ROBERTS, J. / LEWIS, J. / GLICKEN, D. et al. | AIAA | 1985

    New directions in automated spacecraft cost estimation

    PEKAR, P. P. / FRIEDLANDER, A. L. / ROBERTS, D. L. | AIAA | 1975

    AMC-1 (GE-1) Arcjets at 12-Plus Years On-Orbit

    Lichtin, Daniel / Chilelli, N. / Henderson, J. et al. | AIAA | 2009

    Large inclination change using lunar-swingby techniques

    LEE, T. / DUNHAM, D. / HSU, S. et al. | AIAA | 1988

    An analytical method for ride quality of flexible airplanes

    SWAIM, R. L. / SCHMIDT, D. K. / ROBERTS, P. A. et al. | AIAA | 1977

    Jet spoiler as a yaw control device

    TAVELLA, D. A. / LEE, C. S. / WOOD, N. J. et al. | AIAA | 1987

    An Analytical Model for Nitric Oxide Formation in a Gas Turbine Combustor

    RICHARD ROBERTS / LEONARD D. ACETO / REINER KOLLRACK et al. | AIAA | 1972

    Concepts for large interferometers in space

    MORGAN, S. / NEIN, M. / DAVIS, B. et al. | AIAA | 1982

    Material-Aero-Thermal Interaction Computations in the ATLLAS European Programme

    Bouchez, Marc / Cheuret, F. / Grenard, P. et al. | AIAA | 2008

    A parabolized Navier-Stokes prediction of hypersonic window cooling

    BANKEN, G. J. / ROBERTS, D. W. / HOLCOMB, J. E. et al. | AIAA | 1986

    Multi-Level Coupled Simulations of Cooled Structures in the ATLLAS European Program

    Bouchez, Marc / Dufour, Emmanuel / Cheuret, Francois et al. | AIAA | 2009

    Neutralization of beam-emitting spacecraft by plasma injection

    SASAKI, S. / KAWASHIMA, N. / KURIKI, K. et al. | AIAA | 1987

    Materials Exposure and Degradation Experiment (MEDET)

    Tighe, A. / Gabriel, S. / Goulty, D. et al. | AIAA | 2001