Книги з теми "High speed rotor"
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Ознайомтеся з топ-37 книг для дослідження на тему "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.
Знайти повний текст джерелаRutherford, 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.
Знайти повний текст джерелаJohnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. [S.l.]: [s.n.], 1986.
Знайти повний текст джерелаJohnson, 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.
Знайти повний текст джерелаLance, 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.
Знайти повний текст джерелаY, Sung Daniel, Stroub Robert H, and 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.
Знайти повний текст джерелаY, Sung Daniel, Stroub Robert H, and 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.
Знайти повний текст джерелаLance, 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.
Знайти повний текст джерелаY, Sung Daniel, Stroub Robert H, and 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаR, McCarthy Thomas, and 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.
Знайти повний текст джерелаChattopadhyay, Aditi. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаJ, Schneider J., Bartie K. M, and Ames Research Center, eds. Technology needs for high-speed rotorcraft (I). Philadelphia, PA: Boeing Helicopters, 1991.
Знайти повний текст джерелаCenter, Ames Research, and 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.
Знайти повний текст джерелаGahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif: Naval Postgraduate School, 1997.
Знайти повний текст джерелаH, Goldthorpe Steve, and 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.
Знайти повний текст джерелаH, Goldthorpe S., and 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.
Знайти повний текст джерелаG, Steenken W., and 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.
Знайти повний текст джерелаVaez-Zadeh, Sadegh. Rotor Position and Speed Estimation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198742968.003.0006.
Повний текст джерелаNational 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.
Знайти повний текст джерелаPerformance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаWindage Power Loss in Gas Foil Bearings and the Rotor-Stator Clearance of High Speed Generators Operating in High Pressure Environments. Independently Published, 2019.
Знайти повний текст джерелаCost 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.
Знайти повний текст джерелаCost 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.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Optimum Design of High-Speed Prop-Rotors. Independently Published, 2018.
Знайти повний текст джерелаPressure-Sensitive Paint Measurements on a Rotor Disk Surface at High Speeds. Storming Media, 1997.
Знайти повний текст джерелаGuidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаThe selection of convertible engines with current gas generator technology for high speed rotorcraft. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаNational 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.
Знайти повний текст джерелаAn 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.
Знайти повний текст джерелаAn 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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