Books on the topic 'Trailing edge flaps'
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Hassan, A. A. Blade-mounted trailing edge flap control for BVI noise reduction. Langley Research Center, 1992.
Find full textCenter, Langley Research, ed. Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textW, Paulson John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textW, Paulson John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textBanks, Daniel W. Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system. Langley Research Center, 1987.
Find full textApplin, Zachary T. Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textApplin, Zachary T. Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textApplin, Zachary T. Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textGloria, Hernandez, and Langley Research Center, eds. Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textRudolph, Peter K. C. High-lift systems on commercial subsonic airliners. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textApplin, Zachary T. Wing pressure distributions from subsonic tests of a high-wing transport model. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textApplin, Zachary T. Wing pressure distributions from subsonic tests of a high-wing transport model. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textD, Hoffler Keith, and Langley Research Center, eds. A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textM, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.
Find full textFears, Scott P. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50. Langley Research Center, 1995.
Find full textM, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.
Find full textM, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.
Find full textA, Hassan A., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Blade-mounted trailing edge flap control for BVI noise reduction. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textA, Hassan A., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Blade-mounted trailing edge flap control for BVI noise reduction. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textLee, B. H. K. An experimental study of transonic buffet of a supercritical airfoil with trailing edge flap. National Research Council Canada, 1988.
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 textA Three-Dimensional Flutter Theory For Rotor Blades With Trailing-Edge Flaps. Storming Media, 2003.
Find full textBergami, Leonardo. Smart Rotor Modeling: Aero-Servo-Elastic Modeling of a Smart Rotor with Adaptive Trailing Edge Flaps. Springer, 2016.
Find full textBergami, Leonardo. Smart Rotor Modeling: Aero-Servo-Elastic Modeling of a Smart Rotor with Adaptive Trailing Edge Flaps. Springer London, Limited, 2014.
Find full textBergami, Leonardo. Smart Rotor Modeling: Aero-Servo-Elastic Modeling of a Smart Rotor with Adaptive Trailing Edge Flaps. Springer, 2014.
Find full textLow-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Pressure Distributions from Subsonic Tests of an Advanced Laminar-Flow-Control Wing with Leading- and Trailing-Edge Flaps. Independently Published, 2018.
Find full textActive Spanwise Lift Control: A Distributed Parameter Approach. American Institute of Aeronautics & Astronautics, 2020.
Find full textPredicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textHigh-lift systems on commercial subsonic airliners. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textApplication of particle image velocimetry to a study of flow about a multi-element airfoil: Final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155. Dept. of Aeronautics and Astronautics, Stanford University, 1996.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Low Speed Wind Tunnel Investigation of Reynolds Number Effects on a 60-Deg Swept Wing Configuration with Leading and Trailing Edge Flaps. Independently Published, 2018.
Find full textWind-Tunnel Investigation of Control-surface Characteristics: XVI, Pressure Distribution over an NACA 0009 Airfoil with 0. 30-Airfoil-chord Beveled-trailing-edge Flaps. Creative Media Partners, LLC, 2021.
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