101–120 von 288 Ergebnissen
|

    Overview and major characteristics of future aeronautical and space systems

    Venneri, Samuel L. / Noor, Ahmed K. | NTRS | 1992
    A systematic projection is made of prospective materials and structural systems' performance requirements in light of emerging applications ...
    Verlag: NASA National Aeronautics and Space Administration

    Overlay Coatings Technology Development for GRCop-84 Combustion Chamber Liners for Reusable Launch Vehicles

    Nesbitt, James / Raj, Sai / Greenbauer-Seng, Leslie | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics

    Optimum design for double-lap bolted composite joints using a genetic algorithm

    Kradinov, V. / Barut, A. / Madenci, E. et al. | Tema Archiv | 2001
    laminates. Bolt diameters and the spacing between the bolts along the length and width directions of the joint are considered as design variables ...

    Optimum design and testing of a post-buckled stiffened panel

    Lillico, M. / Butler, R. / Hunt, G.W. et al. | Tema Archiv | 2000
    of an initial overall imperfection. The resulting panel has been analyzed using the non-linear FE package ABAQUS and four laboratory ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Optimizing tuning masses for helicopter rotor blade vibration reduction including computed airloads and comparison with test data

    Pritchard, Jocelyn I. / Adelman, Howard M. / Walsh, Joanne L. et al. | NTRS | 1992
    An optimization procedure is developed for locating tuning masses on a rotor blade so that vibratory loads are minimized and hub-shear ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Optimization of Wind Turbine Blade Spars

    Pirrera, Alberto / Capuzzi, Marco / Buckney, Neil et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Optimization of the Wind Turbine Rotor to Enhance the Performance

    Kim, Taeseong / Bak, Christian / Buhl, Thomas | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Optimization of composite engine structures for mechanical and thermal loads

    Kodiyalam, S. / Parthasarathy, V.N. / Hartle, M.S. et al. | Tema Archiv | 1993
    A composites optimization capability for aircraft engine components, for structural and thermal design requirements, is currently under ...

    Optimization of Aircraft Wings Including Dynamic Aeroelasticity and Manufacturing Aspects

    Petersson, O. | British Library Conference Proceedings | 2009
    Schlagwörter: Materials , Structural dynamics

    Optimal Terminal Trajectory Control of Vertically Stroking Crew Seats Using MREAs

    Singh, Harinder / Choi, Young / Wereley, Norman | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    On the use of component modes in multibody dynamics

    Craig, R.R. jun. / Anthony, T.C. | Tema Archiv | 1996
    characterize the elastic deformation of the articulating component. Analysis of the dynamics of spacecraft with articulating appendages, robots, and ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston
    Schlagwörter: Dynamik

    On the Effects of Structural Modifications in the Large Wind Turbine Dynamics

    Coppotelli, Giuliano / Balis Crema, Luigi / Grappasonni, Chiara | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    On-Condition Evaluation of How Inertial and Aerodynamic Characteristics Affect the Dynamics of a Small Wind Turbine System

    Grappasonni, Chiara / Coppotelli, Giuliano / Arsenault, Tyler et al. | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

    Numerical modeling of creep in polymer matrix composites with transverse isotropy

    Acharya, S. / Binienda, W. / Robinson, D. | Tema Archiv | 2003
    commercially available code and was able to predict creep, deformation/damage phenomena in a Finite Element Model. As such, the code requires material ...
    Schlagwörter: Kriechen (Werkstoff)

    Nonlinear analysis of the space shuttle super-lightweight external fuel tank

    Nemeth, M.P. / Britt, V.O. / Collins, T.J. et al. | Tema Archiv | 1996
    . Modeling details and results are presented for two prelaunch loading conditions and for two full-scale structural tests that were conducted on the ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Nonlinear Analysis and Post-Test Correlation for a Curved PRSEUS Panel

    Gould, Kevin / Lovejoy, Andrew E. / Jegley, Dawn et al. | NTRS | 2013
    panel using a full-scale curved panel in the FAA Full-Scale Aircraft Structural Test Evaluation and Research (FASTER) facility. Testing was ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects

    Lee, Dong-Hwan / Chen, P. C. | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    Nonlinear Aeroelastic Scaling of a Joined Wing Aircraft

    Ricciardi, Anthony / Canfield, Robert / Patil, Mayuresh et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Nonlinear Aeroelastic Power Flow Control for Wind Turbines

    Robinett, Rush / Wilson, David | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft

    Patil, Mayuresh | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics