Books on the topic 'Rotors (Helicopters)'

Gilliand, Harry E. Dancing rotors. Arlington, Tex: Aerofax, 1994.

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.

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.

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.

Runyan, Harry L. Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight. Washington: NASA, 1985.

H, Tai, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Compressible, unsteady, lifting-surface theory for a helicopter rotor in forward flight. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Maskew, Langley Research Center, and Analytical Methods Inc, eds. Inviscid analysis of unsteady blade tip flow correlation studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Application of higher harmonic blade feathering on the OH-6A helicopter for vibration reduction. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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.

Mutza, Wayne. Bent & battered rotors. Carrollton, TX: Squadron/Signal Publications, 1993.

Center, Ames Research, ed. A survey of theoretical and experimental coaxial rotor aerodynamic research. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

Center, Ames Research, ed. A survey of theoretical and experimental coaxial rotor aerodynamic research. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

Coleman, Colin P. A survey of theoretical and experimental coaxial rotor aerodynamic research. Washington, D.C: National Aeronautics and Space Administration, 1997.

Center, Ames Research, ed. The acoustics of a small-scale helicopter rotor in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Center, Ames Research, ed. The evaluation of a number of prototypes for the free-tip rotor constant-moment controller. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center., 1987.

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

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. Preliminary structural design of composite main rotor blades for minimum weight. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

United States. National Aeronautics and Space Administration., ed. Ongoing development of a computer jobstream to predict helicopter main rotor performance in icing conditions. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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.

A, Young Larry, Signor David B, and Ames Research Center, eds. Performance and loads data from a hover test of a full-scale advanced technology XV-15 rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

A, Young Larry, Signor David B, and Ames Research Center, eds. Performance and loads data from a hover test of a full-scale advanced technology XV-15 rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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

Center, Ames Research, ed. The acoustics of a small-scale helicopter rotor in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

R, Groepler David, and Ames Research Center, eds. Tiltrotor research aircraft composite blade repairs: Lessons learned. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

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.

J, Madden Joseph, and Ames Research Center, eds. Rotor and control system loads analysis of the XV-15 with the advanced technology blades. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

Wayne, Johnson, and Ames Research Center, eds. Correlation of airloads on a two-bladed helicopter rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

J, Collins Leslie, and Ames Research Center, eds. An evaluation of three helicopter rotor sections. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

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.

D, Betzina Mark, Signor David B, and Ames Research Center, eds. Performance and loads data from a hover test of a full-scale XV-15 rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Center, Ames Research, ed. The acoustics of a small-scale helicopter rotor in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Mihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Mihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. Cleveland, Ohio: Lewis Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Integration of dynamic, aerodynamic, and structural optimization of helicopter rotor blades: Second semi-annual status report NASA research grant no. NAG 1-710 for period covering 14 April 1987 to 13 October 1987. [Washington, DC: National Aeronautics and Space Administration, 1987.

Mihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

M, McKillip R., and United States. National Aeronautics and Space Administration., eds. Coupled rotor-body equations of motion hover flight: Interim report. Princeton, NJ: Dept. of Mechanical and Aerospace Engineering, Princeton University, 1990.

Transportation Safety Board of Canada. Tail rotor drive shaft failure, Great Slave Helicopters Ltd., Bell 206B JetRanger (Helicopter) C-FHZJ, Yellowknife, Northwest Territories 45 nm NM, 29 September 1993. Hull, Quebec: Transportation Safety Board of Canada, 1994.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

J, Decker Harry, Shimski John T, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Center, Ames Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Control of helicopter rotorblade aerodynamics. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Estimation of blade airloads from rotor blade bending moments. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

1936-, Tung C., United States. Army Aviation Systems Command., and Ames Research Center, eds. Finite-difference computations of rotor loads. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

Althoff, Susan L. Effect of blade planform variation on a small-scale hovering rotor. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.