Books on the topic '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.
Find full textUnited 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.
Find full textUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Helicopter blade-vortex interaction noise with comparisons to CFD calculations. National Aeronautics and Space Administration, 1996.
Find full textKen, Duisenberg, and Ames Research Center, eds. Simulation of rotor blade element turbulence. National Aeronautics and Space Administration, Ames Research Center, 1995.
Find full textAlan, 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.
Find full textAlan, 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.
Find full textAlan, 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.
Find full textCenter, Langley Research, ed. Full-potential modeling of blade-vortex interactions. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textCenter, Langley Research, ed. Full-potential modeling of blade-vortex interactions. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textL, 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.
Find full textUnited 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.
Find full textLtd, Nor'wester Energy Systems. Wind turbine rotor blade contamination and effects on performance: A study. The Branch, 1989.
Find full textChen, C. L. Numerical simulation of helicopter multi-bladed rotor flow. American Institute of Aeronautics and Astronautics, 1988.
Find full textCenter, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textCenter, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textRobinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Naval Postgraduate School, 1997.
Find full textKretz, Allan. Measured and simulated turbulence: Compared at a section of a rotating wind turbine blade. Risø National Laboratory, 1994.
Find full textG, 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.
Find full textUnited 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.
Find full textS, 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.
Find full textYeager, William T. Wind-tunnel evaluation of an advanced main-rotor blade design for a utility-class helicopter. Langley Research Center, 1987.
Find full textT, 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.
Find full textSingleton, 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.
Find full textBir, Gunjit S. Structural design of a horizontal-axis tidal current turbine composite blade. National Renewable Energy Laboratory, 2011.
Find full textMiller, 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.
Find full textChattopadhyay, Aditi. An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades. Langley Research Center, 1990.
Find full textH, 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.
Find full textMillott, T. A. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade. Ames Research Center, 1994.
Find full textHounjet, M. H. L. A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies. National Aerospace Laboratory, 1985.
Find full textHeidelberg, Laurence J. Advanced turboprop wing installation effects measured by unsteady blade pressure and noise. National Aeronautics and Space Administration, 1987.
Find full textS, 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.
Find full textS, 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.
Find full textUnited 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.
Find full textUnited 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.
Find full textCorrigan, 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.
Find full textBerry, 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.
Find full textN, 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.
Find full textHand, M. Maureen. Mitigation of wind turbine/vortex interaction using disturbance accommodating control. National Renewable Energy Laboratory, 2003.
Find full textCenter, Ames Research, ed. Design and manufacture of wood blades for windtunnel fans. National Aeronautics and Space Administration, Ames Research Center, 1998.
Find full textCenter, Ames Research, ed. Design and manufacture of wood blades for windtunnel fans. National Aeronautics and Space Administration, Ames Research Center, 1998.
Find full textE, 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.
Find full textDunn, Mark H. The solution of a singular integral equation arising from a lifting surface theory for rotating blades. Old Dominion University, 1991.
Find full textKlein, William E. Model 0A wind turbine generator FMEA. National Aeronautics and Space Administration, 1989.
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