Libros sobre el tema "High speed rotor"
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Huppunen, Jussi. High-speed solid-rotor induction machine: Electromagnetic calculation and design. Lappeenranta: Lappeenranta University of Technology, 2004.
Buscar texto completoRutherford, John W. Shock fitting applied to the prediction of high-speed rotor noise. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.
Buscar texto completoJohnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. [S.l.]: [s.n.], 1986.
Buscar texto completoJohnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.
Buscar texto completoLance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Buscar texto completoY, Sung Daniel, Stroub Robert H y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Buscar texto completoY, Sung Daniel, Stroub Robert H y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Buscar texto completoLance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. Hampton, Va: Langley Research Center, 1991.
Buscar texto completoY, Sung Daniel, Stroub Robert H y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Buscar texto completoUnited States. Congress. Office of Technology Assessment., ed. New ways: Tiltrotor aircraft and magnetically levitated vehicles. Washington, DC: Congress of the U.S., Office of Technology Assessment, 1991.
Buscar texto completoR, McCarthy Thomas y United States. National Aeronautics and Space Administration., eds. An integrated optimum design approach for high speed prop rotors: Final report on NASA Ames grant no. NCC2-795. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Buscar texto completoChattopadhyay, Aditi. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Buscar texto completoJ, Schneider J., Bartie K. M y Ames Research Center, eds. Technology needs for high-speed rotorcraft (I). Philadelphia, PA: Boeing Helicopters, 1991.
Buscar texto completoCenter, Ames Research y United States. Army Aviation Research and Technology Activity., eds. Wake model for helicopter rotors in high speed flight. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Buscar texto completoGahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif: Naval Postgraduate School, 1997.
Buscar texto completoH, Goldthorpe Steve y Langley Research Center, eds. Guidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Buscar texto completoH, Goldthorpe S. y Langley Research Center, eds. Guidance and control design for high-speed rollout and turnoff (ROTO): Contract NAS1-19703. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Buscar texto completoG, Steenken W. y Hugh L. Dryden Flight Research Center., eds. Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Buscar texto completoVaez-Zadeh, Sadegh. Rotor Position and Speed Estimation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198742968.003.0006.
Texto completoNational Aeronautics and Space Administration (NASA) Staff. Low-Speed Wind-Tunnel Test of an Unpowered High-Speed Stoppable Rotor Concept in Fixed-Wing Mode. Independently Published, 2018.
Buscar texto completoPerformance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Buscar texto completoA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Buscar texto completoA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Buscar texto completoWindage Power Loss in Gas Foil Bearings and the Rotor-Stator Clearance of High Speed Generators Operating in High Pressure Environments. Independently Published, 2019.
Buscar texto completoCost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Moffett Field, CA: Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.
Buscar texto completoCost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Moffett Field, CA: Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.
Buscar texto completoNational Aeronautics and Space Administration (NASA) Staff. Optimum Design of High-Speed Prop-Rotors. Independently Published, 2018.
Buscar texto completoPressure-Sensitive Paint Measurements on a Rotor Disk Surface at High Speeds. Storming Media, 1997.
Buscar texto completoGuidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Buscar texto completoThe selection of convertible engines with current gas generator technology for high speed rotorcraft. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Buscar texto completoNational Aeronautics and Space Administration (NASA) Staff. Optimum Design of High Speed Prop Rotors Including the Coupling of Performance, Aeroelastic Stability and Structures. Independently Published, 2018.
Buscar texto completoAn integrated optimum design approach for high speed prop rotors: Final report on NASA Ames grant no. NCC2-795. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Buscar texto completoAn Integrated optimum design approach for high speed prop-rotors including acoustic constraints: Semi-annual progress report ... January 1 - June 30, 1993. [Washington, DC: National Aeronautics and Space Administration, 1993.
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