Książki na temat „Winged blade”
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Bir, Gunjit S. User's guide to MBC3: Multi-blade coordinate transformation code for 3-bladed wind turbines. National Renewable Energy Laboratory, 2010.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions. National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Znajdź pełny tekst źródłaKen, Duisenberg, and Ames Research Center, eds. Simulation of rotor blade element turbulence. National Aeronautics and Space Administration, Ames Research Center, 1995.
Znajdź pełny tekst źródłaAlan, Egolf T., and Langley Research Center, eds. Evaluation of a doubly-swept blade tip for rotorcraft noise reduction. National Aeronautics and Space Administration, Langley Research Center, 1992.
Znajdź pełny tekst źródłaAlan, Egolf T., and Langley Research Center, eds. Evaluation of a doubly-swept blade tip for rotorcraft noise reduction. National Aeronautics and Space Administration, Langley Research Center, 1992.
Znajdź pełny tekst źródłaAlan, Egolf T., and Langley Research Center, eds. Evaluation of a doubly-swept blade tip for rotorcraft noise reduction. National Aeronautics and Space Administration, Langley Research Center, 1992.
Znajdź pełny tekst źródłaCenter, Langley Research, ed. Full-potential modeling of blade-vortex interactions. National Aeronautics and Space Administration, Langley Research Center, 1997.
Znajdź pełny tekst źródłaCenter, Langley Research, ed. Full-potential modeling of blade-vortex interactions. National Aeronautics and Space Administration, Langley Research Center, 1997.
Znajdź pełny tekst źródłaL, Walsh Joanne, Young Katherine C, and United States. National Aeronautics and Space Administration., eds. Application of response surface techniques to helicopter rotor blade optimization procedure. National Aeronautics and Space Administration, 1995.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., ed. Design and fabrication of forward-swept counterrotation blade configuration for wind tunnel testing: Final report. National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaLtd, Nor'wester Energy Systems. Wind turbine rotor blade contamination and effects on performance: A study. The Branch, 1989.
Znajdź pełny tekst źródłaChen, C. L. Numerical simulation of helicopter multi-bladed rotor flow. American Institute of Aeronautics and Astronautics, 1988.
Znajdź pełny tekst źródłaCenter, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.
Znajdź pełny tekst źródłaCenter, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.
Znajdź pełny tekst źródłaRobinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Naval Postgraduate School, 1997.
Znajdź pełny tekst źródłaKretz, Allan. Measured and simulated turbulence: Compared at a section of a rotating wind turbine blade. Risø National Laboratory, 1994.
Znajdź pełny tekst źródłaG, Bousman William, U.S. Army Aviation and Troop Command., and Ames Research Center, eds. An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis. US Army Aviation and Troop Command, 1993.
Znajdź pełny tekst źródłaUnited States. Army. Aerostructures Directorate. and Langley Research Center, eds. Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Znajdź pełny tekst źródłaS, Wittmer Kenneth, Wenger Christian W, and United States. National Aeronautics and Space Administration., eds. The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction: Final technical report ... Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, 1997.
Znajdź pełny tekst źródłaYeager, William T. Wind-tunnel evaluation of an advanced main-rotor blade design for a utility-class helicopter. Langley Research Center, 1987.
Znajdź pełny tekst źródłaT, Yeager William, Wilbur Matthew L, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Znajdź pełny tekst źródłaSingleton, Jeffrey D. Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Znajdź pełny tekst źródłaBir, Gunjit S. Structural design of a horizontal-axis tidal current turbine composite blade. National Renewable Energy Laboratory, 2011.
Znajdź pełny tekst źródłaMiller, Dean R. Analytical model for predicting emergency shutdown of a two-blade d horizontal axis wind turbine. U.S. Dept. Energy, Wind Energy Technology Division, 1985.
Znajdź pełny tekst źródłaChattopadhyay, Aditi. An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades. Langley Research Center, 1990.
Znajdź pełny tekst źródłaH, Mirick Paul, Langston Chester W, and Langley Research Center, eds. Rotating shake test and modal analysis of a model helicopter rotor blade. National Aeronautics and Space Administration, Langley Research Center, 1997.
Znajdź pełny tekst źródłaMillott, T. A. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade. Ames Research Center, 1994.
Znajdź pełny tekst źródłaHounjet, M. H. L. A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies. National Aerospace Laboratory, 1985.
Znajdź pełny tekst źródłaHeidelberg, Laurence J. Advanced turboprop wing installation effects measured by unsteady blade pressure and noise. National Aeronautics and Space Administration, 1987.
Znajdź pełny tekst źródłaS, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaS, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaUnited States. Dept. of Energy. Wind/Ocean Technologies Division. and Lewis Research Center, eds. Mod-2 wind turbine field operations experience. National Aeronautics and Space Administration, Lewis Research Center, 1985.
Znajdź pełny tekst źródłaUnited States. Dept. of Energy. Wind/Ocean Technologies Division. and Lewis Research Center, eds. Mod-2 wind turbine field operations experience. National Aeronautics and Space Administration, Lewis Research Center, 1985.
Znajdź pełny tekst źródłaCorrigan, Robert D. Design and initial testing of a one-bladed 30-meter rotor on the NASA-DIE Mod-o wind turbine. National Aeronautics and Space Administration, 1986.
Znajdź pełny tekst źródłaBerry, John D. Helicopter blade dynamic loads measured during performance testing of two scaled rotors. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Znajdź pełny tekst źródłaN, Duque Earl P., and United States. National Aeronautics and Space Administration., eds. Helicopter rotor blade computation in unsteady flows using moving overset grids. American Institute of Aeronautics and Astronautics, 1996.
Znajdź pełny tekst źródłaHand, M. Maureen. Mitigation of wind turbine/vortex interaction using disturbance accommodating control. National Renewable Energy Laboratory, 2003.
Znajdź pełny tekst źródłaCenter, Ames Research, ed. Design and manufacture of wood blades for windtunnel fans. National Aeronautics and Space Administration, Ames Research Center, 1998.
Znajdź pełny tekst źródłaCenter, Ames Research, ed. Design and manufacture of wood blades for windtunnel fans. National Aeronautics and Space Administration, Ames Research Center, 1998.
Znajdź pełny tekst źródłaE, Simley, Pao L. Y, and National Renewable Energy Laboratory (U.S.), eds. LIDAR wind speed measurement analysis and feed-forward blade pitch control for load mitigation in wind turbines: January 2010 - January 2011. National Renewable Energy Laboratory, 2011.
Znajdź pełny tekst źródłaDunn, Mark H. The solution of a singular integral equation arising from a lifting surface theory for rotating blades. Old Dominion University, 1991.
Znajdź pełny tekst źródłaKlein, William E. Model 0A wind turbine generator FMEA. National Aeronautics and Space Administration, 1989.
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