Books on the topic 'Rotors (Helicopters) - Models'

B, Connor Andrew, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Wind-tunnel acoustic results of two rotor models with several tip designs. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Connor Andrew, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Wind-tunnel acoustic results of two rotor models with several tip designs. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Connor Andrew, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Wind-tunnel acoustic results of two rotor models with several tip designs. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Murthy, V. R. Comprehensive analysis of helicopters with bearingless rotors: Status report. Syracuse, N.Y: Syracuse University, Dept. of Mechanical and Aerospace Engineering, 1988.

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: Ames Research Center, 1989.

Berry, John D. Helicopter blade dynamic loads measured during performance testing of two scaled rotors. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 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, 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.

Y, 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.

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, 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.

Peretz, Friedmann, Kosmatka J. B, American Society of Mechanical Engineers. Aerospace Division., and American Society of Mechanical Engineers. Winter Meeting, eds. Recent advances in the structural dynamic modeling of composite rotor blades and thick composites: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Anaheim, California, November 8-13, 1992. New York: ASME, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Takahashi, Marc D. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. Moffett Field, Calif: NASA Ames Research Center, 1990.

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. Hampton, Va: Langley Research Center, 1988.

Ralph, Jolly J., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Martin, R. M. Acoustic test of a model rotor and tail rotor: Results for the isolated rotors and combined configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Facility, Dryden Flight Research, ed. Higher harmonic control analysis for vibration reduction of helicopter rotor systems. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1994.

Facility, Dryden Flight Research, ed. Higher harmonic control analysis for vibration reduction of helicopter rotor systems. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1994.

Miller, Thomas L. Icing research tunnel test of a model helicopter rotor. [Washington, DC]: National Aeronautics and Space Administration, 1989.

E, Bassett D., and Ames Research Center, eds. Application of a Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics (CAMRAD) to the McDonnell Douglas AH-64A helicopter. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Helicopter blade-vortex interaction locations: Scale-model acoustics and free-wake analysis results. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Helicopter blade-vortex interaction locations: Scale-model acoustics and free-wake analysis results. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. Effect of planform taper on hover performance of an advanced AH-64 model rotor. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

W, Kohlhepp F., Leighton K. P, and Ames Research Center, eds. Acoustic characteristics of 1/20-scale model helicopter rotors. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1986.

Hoad, Danny R. Helicopter blade-vortex interaction locations - scale-model acoustics and free-wake analysis results. Hampton, Va: Langley Research Center, 1987.

Center, Langley Research, and United States. Army Aviation Systems Command., eds. Stress analysis of 27% scale model of AH-64 main rotor hub. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

A, Young Larry, and Ames Research Center, eds. The results of a wind tunnel investigation of a model rotor with a free tip. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, 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.

Allen, Dale, Lorber Peter, and Ames Research Center, eds. Wind tunnel test of a variable-diameter tiltrotor (VDTR) model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

R, Mantay Wayne, and Langley Research Center, eds. Aeroelastic model helicopter rotor testing in the Langley TDT. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

R, Mantay Wayne, and Langley Research Center, eds. Aeroelastic model helicopter rotor testing in the Langley TDT. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

C, Curtiss H., and United States. National Aeronautics and Space Administration., eds. An analytic modeling and system identification study of rotor/fuselage dynamics at hover. [Washington, DC: National Aeronautics and Space Administration, 1993.

Brentner, Kenneth S. A prediction of helicopter rotor discrete frequency noise for three scale models using a new acoustics program. New York: AIAA, 1987.

A, Boxwell D., Spencer R. H, Ames Research Center, and United States. Army Aviation Research and Technology Activity., eds. Review and analysis of the DNW/model 360 rotor acoustic data base. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Chaffin, Mark S. A guide to the use of the pressure disk rotor model as implemented in INS3D-UP. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Tradelius, Paul. Model airplane news presents the basics of RC helis: The ultimate guide to rotary flight. Ridgefield, CT: Air Age Media, 2006.

Tradelius, Paul. Model airplane news presents the basics of RC helis: The ultimate guide to rotary flight. Ridgefield, CT: Air Age Media, 2006.

H, Mirick Paul, Langston Chester W, and Langley Research Center, eds. Rotating shake test and modal analysis of a model helicopter rotor blade. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Mineck, Raymond E. Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Berry, John D. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, and U.S. Army Aviation and Troop Command., eds. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

N, Duque Earl P., and United States. National Aeronautics and Space Administration., eds. Helicopter rotor blade computation in unsteady flows using moving overset grids. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

H, Hamouda M.-Nabil, Yeager William T, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

H, Hamouda M.-Nabil, Yeager William T, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Mirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.