Livres sur le sujet « High speed rotor »

Huppunen, Jussi. High-speed solid-rotor induction machine : Electromagnetic calculation and design. Lappeenranta : Lappeenranta University of Technology, 2004.

Rutherford, 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.

Johnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. [S.l.] : [s.n.], 1986.

Johnson, 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.

Lance, 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.

Y, Sung Daniel, Stroub Robert H et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.

Y, Sung Daniel, Stroub Robert H et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.

Lance, 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.

Y, Sung Daniel, Stroub Robert H et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.

United States. National Aeronautics and Space Administration., dir. Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC] : National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., dir. 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.

United States. National Aeronautics and Space Administration., dir. 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.

United States. Congress. Office of Technology Assessment., dir. New ways : Tiltrotor aircraft and magnetically levitated vehicles. Washington, DC : Congress of the U.S., Office of Technology Assessment, 1991.

R, McCarthy Thomas, et United States. National Aeronautics and Space Administration., dir. 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.

Chattopadhyay, Aditi. Optimum design of high speed prop-rotors. [Washington, DC : National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., dir. Optimum design of high speed prop-rotors. [Washington, DC : National Aeronautics and Space Administration, 1992.

J, Schneider J., Bartie K. M et Ames Research Center, dir. Technology needs for high-speed rotorcraft (I). Philadelphia, PA : Boeing Helicopters, 1991.

Center, Ames Research, et United States. Army Aviation Research and Technology Activity., dir. Wake model for helicopter rotors in high speed flight. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.

Gahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif : Naval Postgraduate School, 1997.

H, Goldthorpe Steve, et Langley Research Center, dir. Guidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1995.

H, Goldthorpe S., et Langley Research Center, dir. 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.

G, Steenken W., et Hugh L. Dryden Flight Research Center., dir. 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.

Vaez-Zadeh, Sadegh. Rotor Position and Speed Estimation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198742968.003.0006.

National 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.

Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC] : National Aeronautics and Space Administration, 1996.

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.

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.

Windage Power Loss in Gas Foil Bearings and the Rotor-Stator Clearance of High Speed Generators Operating in High Pressure Environments. Independently Published, 2019.

Cost 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.

Cost 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.

National Aeronautics and Space Administration (NASA) Staff. Optimum Design of High-Speed Prop-Rotors. Independently Published, 2018.

Pressure-Sensitive Paint Measurements on a Rotor Disk Surface at High Speeds. Storming Media, 1997.

Guidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1995.

The selection of convertible engines with current gas generator technology for high speed rotorcraft. [Washington, DC] : National Aeronautics and Space Administration, 1991.

National 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.

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.

An 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.