Książki na temat „COMPOSITE ROTOR”

Piatak, David J. Stiffness characteristics of composite rotor blades with elastic couplings. Washington, D.C: National Aeronautics and Space Administration, 1997.

W, Nixon Mark, Kosmatka J. B i Langley Research Center, red. Stiffness characteristics of composite rotor blades with elastic couplings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Moura, Geraldo A. Macedo. An approach for design and analysis of composite rotor blades. Monterey, Calif: Naval Postgraduate School, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., red. 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.

W, Nixon Mark, Rehfield Lawrence W i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Comparison of composite rotor blade models: A coupled-beam analysis and an MSC/NASTRAN finite-element model. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration., red. Aeroelastic response and stability of tiltrotors with elastically-coupled composite rotor blades. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, Langley Research, red. Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

United States. National Aeronautics and Space Administration., red. Aeroelastic response and stability of tiltrotors with elastically-coupled composite rotor blades. [Washington, DC: National Aeronautics and Space Administration, 1993.

Lake, Renee C. Experimental and analytical investigation of dynamic characteristics of extension-twist-coupled composite tubular spars. Hampton, Va: Langley Research Center, 1993.

C, Park K., i Langley Research Center, red. An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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

Peretz, Friedmann, Kosmatka J. B, American Society of Mechanical Engineers. Aerospace Division. i American Society of Mechanical Engineers. Winter Meeting, red. 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., red. Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corp., 1986.

United States. National Aeronautics and Space Administration., red. Wing design for a civil tiltrotor transport aircraft: Performance report for the period of (1-25-94 to 11-24-94) grant no. NAG-1-1571. [Washington, DC: National Aeronautics and Space Administration, 1994.

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

Y, Baaklini George, i NASA Glenn Research Center, red. Ultrasonic resonance spectroscopy of composite rims for flywheel rotors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Y, Baaklini George, i NASA Glenn Research Center, red. Ultrasonic resonance spectroscopy of composite rings for flywheel rotors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Harmon, Laura M. Ultrasonic resonance spectroscopy of composite rings for flywheel rotors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Center, Langley Research, red. Flight service evaluation of composite helicopter components: Final report February 1981 through November 1990. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

D, Schnittgrund Gary, Rockwell International Rocketdyne Division i Lewis Research Center, red. Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines: Phase I, final report. Canoga Park, CA: Rocketdyne Division, Rockwell International, 1990.

D, Schnittgrund Gary, Rockwell International Rocketdyne Division i Lewis Research Center, red. Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines: Phase I, final report. Canoga Park, CA: Rocketdyne Division, Rockwell International, 1990.

R, Carluccio J., Norman J. P i United States. National Aeronautics and Space Administration., red. The application of cast SiC/Al to rotary engine components. [Washington, D.C: National Aeronautics and Space Administration, 1986.

A preliminary investigation of finite-element modeling for composite rotor blades. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Analysis, design and elastic tailoring of composite rotor blades: Final report. Atlanta, Ga: Center for Rotary Wing Aircraft Technology, Georgia Institute of Technology, 1987.

National Aeronautics and Space Administration (NASA) Staff. Aeroelastic Analysis of Helicopter Rotor Blades Incorporating Piezoelectric Fiber Composite Twist Actuation. Independently Published, 2018.

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.

Friedmann, Peretz. Recent Advances in the Structural Dynamic Modeling of Composite Rotor Blades and Thick Composites: Presented at the Winter Annual Meeting of the Ameri (AMD). American Society of Mechanical Engineers, 1992.

National Aeronautics and Space Administration i NASA. Preliminary Design Study of Advanced Composite Blade and Hub and Nonmechanical Control System for the Tilt-Rotor Aircraft - Volume 2 : Project Planning Data: February 1 1980. Independently Published, 2022.

Performance Analysis on Wear and Friction Characteristics of Brake Rotor Made of A359-B4c Composites. Tiruchengode, India: ASDF International, 2017.

Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines: Phase I, final report. Canoga Park, CA: Rocketdyne Division, Rockwell International, 1990.