1–50 von 1,006 Ergebnissen
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    Satellite Formation Control using Differential Drag

    Omar, Sanny R. / Wersinger, J. M. | AIAA | 2015

    A New State-of-The-Art in AF-M315E Thruster Technologies

    Masse, R. / Overly, J. / Allen, M. et al. | AIAA | 2012

    Numerical Study of Cryogenic Jets Under Supercritical Conditions

    J. M. M. Barata / A. R. R. Silva | AIAA | 2003

    Thermal Joint Resistances of Conforming Rough Surfaces with Gas Filled Caps

    M. Bahrami / M. Yovanovich / J. R. Culham | AIAA | 2004

    Validation of a Jet–Surface Interaction Noise Model in Flight

    Dawson, M. F. / Lawrence, J. L. T. / Self, R. H. et al. | AIAA | 2020

    Scaling and Balancing for High-Performance Computation of Optimal Controls

    Ross, I. M. / Gong, Q. / Karpenko, M. et al. | AIAA | 2018

    Validation of New Formulations for Propeller Analysis

    Morgado, J. / Silvestre, M. Â. R. / Páscoa, J. C. | AIAA | 2014

    Wall-Distance-Free Version of Spalart–Allmaras Turbulence Model

    Rahman, M. M. / Agarwal, R. K. / Lampinen, M. J. et al. | AIAA | 2015

    Experimental Characterization of Thermal Wadis in Support of Lunar Exploration

    Matyas, J. / Wegeng, R. / Robinson, M. et al. | AIAA | 2011

    Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads

    Kim, Y. I. / Park, G. J. / Kolonay, R. M. et al. | AIAA | 2008

    Thermal Contact Resistance of Nonconforming Rough Surfaces, Part 2: Thermal Model

    M. Bahrami / J. R. Culham / M. Yovanovich et al. | AIAA | 2004

    Effects of GH/LOX Velocity and Momentum Ratios on Shear Coaxial Injector Atomization

    M. Ferraro / R. J. Kujala / J.-L. Thomas et al. | AIAA | 2002

    Efficient 3D Stress Capture of Variable-Stiffness and Sandwich Beam Structures

    Patni, M. / Minera, S. / Groh, R. M. J. et al. | AIAA | 2019

    Composite Blade Twist Modification by Using a Moving Mass and Stiffness Tailoring

    Amoozgar, M. R. / Shaw, A. D. / Zhang, J. et al. | AIAA | 2018

    Nonlinear Model Reduction of von Kármán Plates Under Linearized Compressible Fluid Flow

    Brake, M. R. / Barone, M. F. / Segalman, D. J. | AIAA | 2012

    Doublet-panel method for half-model wind-tunnel corrections

    MOKRY, M. / DIGNEY, J. R. / POOLE, R. J. D. | AIAA | 1987

    Evaluating Liftoff Debris for NASA’s Space Launch System (SLS) Prior to the Artemis I Launch

    Hays, Michael J. / Robinson, Jennifer R. / Herron, Andrew J. et al. | AIAA | 2024

    Symmetry Properties of the Transitional Sphere Wake

    R. Mittal / J. J. Wilson / F. M. Najjar | AIAA | 2002

    Material model for composites using neural networks

    PIDAPARTI, R. M. V. / PALAKAL, M. J. | AIAA | 1993

    Envelope function - A tool for analyzing flutter data

    COOPER, J. E. / EMMETT, P. R. / WRIGHT, J. R. et al. | AIAA | 1993

    Flow over a twin-tailed aircraft at angle of attack. II - Temporal characteristics

    KOMERATH, N. M. / SCHWARTZ, R. J. / KIM, J. M. | AIAA | 1992

    A State Estimation Approach for High Angle-of-Attack Parameter Estimation from Certification Flight Data

    Leung, Jordan M. / Moszczynski, Gregory J. / Grant, Peter R. | AIAA | 2019

    GOLauncher 1 Hypersonic Testbed

    Piplica, Anthony J. / Olds, John R. / Hellman, Barry M. | AIAA | 2015

    Discrete vortex computation of separated airfoil flow

    BASUKI, J. / GRAHAM, J. M. R. | AIAA | 1987

    Models of space-averaged energetics of plates

    BOUTHIER, O. M. / BERNHARD, R. J. | AIAA | 1992

    Spreading Resistance of Isoflux Rectangles and Strips on Compound Flux Channels

    M. M. Yovanovich / Y. S. Muzychka / J. R. Culham | AIAA | 1999

    Comparative Study of CorrosionFatigue in Aircraft Materials

    Q. Y. Wang / R. M. Pidaparti / M. J. Palakal | AIAA | 2001

    Development of the F/A-18A automatic carrier landing system

    URNES, J. M. / HESS, R. K. | AIAA | 1985

    Boundary Layer Transit Flight Experiment: Mission Overview, Launch Vehicle and Payload Subsystems

    Hörschgen-Eggers, M. / Kirchhartz, R. M. / Jung, W. et al. | AIAA | 2020

    Drag balance for hypervelocity impulse facilities

    SIMMONS, J. M. / SANDERSON, S. R. | AIAA | 1991

    Three-Component Force Measurements on a Large Scramjet in a Shock Tunnel

    M. J. Robinson / D. J. Mee / C. Y. Tsai et al. | AIAA | 2005

    A detailed numerical model of a supersonic reacting mixing layer

    DRUMMOND, J. / ROGERS, R. / HUSSAINI, M. | AIAA | 1986