Books on the topic 'Rotors – Aerodynamics'

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

Aerodynamics of wind turbines: Rotors, loads and structure. London: James X James [i.e. James & James], 2000.

Cross, Jeffrey L. Tip aerodynamics and acoustics test: A report and data survey. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Beesten, Benno. Nichtplanare Rotorblattspitzen im Hubschraubervorwärtsflug. Göttingen: Cuvillier, 1996.

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.

Kroll, Norbert. Berechnung von Strömungsfeldern um Propeller und Rotoren im Schwebeflug durch die Lösung der Euler-Gleichungen. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1989.

Roberts, Thomas W. Euler equation computations for the flow over a hovering helicopter rotor. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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.

Kitaplioglu, Cahit. Analysis of small-scale rotor hover performance data. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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.

Kolokolov, S. N. Dinamika upravli͡a︡emogo dvizhenii͡a︡ vertoleta. Moskva: "Mashinostroenie", 1987.

Kunz, Donald L. Analytical modeling of helicopter static and dynamic induced velocity in grasp. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 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.

Kunz, Donald L. Analytical modeling of helicopter static and dynamic induced velocity in grasp. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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

Chattopadhyay, Aditi. Performance of an optimized rotor blade at off-design flight conditions. Washington, DC: National Aeronautics and Space Administration, 1990.

Berry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.

Berry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.

Berry, John D. Flapping inertia for selected rotor blades. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Berry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.

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

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Rostafiński, Wojciech. Analysis of fully stalled compressor. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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.

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Norman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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.

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.

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.

Center, Ames Research, and Monterey Technologies Inc, eds. Introduction to autogyros, helicopters, and other V/STOL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2011.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Transonic flow analysis for rotors. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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.

Center, Ames Research, ed. Tilt rotor hover aeroacoustics. [Moffett Field, Calif.]: National Aeronautics and Space Administration, Ames Research Center, 1992.

Aerodynamic parameter studies and sensitivity analysis for rotor blades in axial flight. Hampton, Va: Lockheed Engineering & Science Co., 1991.

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.

Sheng, Chunhua. Advances in Transitional Flow Modeling: Applications to Helicopter Rotors. Springer London, Limited, 2016.

Wang, Jingyu, and Chunhua Sheng. Advances in Transitional Flow Modeling: Applications to Helicopter Rotors. Springer International Publishing AG, 2016.

Patrick, Sparks S., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. A full potential flow analysis with realistic wake influence for helicopter rotor airload prediction. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.

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.

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.

Center, Ames Research, ed. The calculation of rotor/fuselage interaction for two-dimensional bodies. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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.

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.

Cooperative agreement #NCC 2-175 entitled Investigation of a free-tip rotor configuration for research on spanwise life [i.e. lift] distributions and wake velocity surveys of a semi-span wing with a discontinuous twist: Final report. Lawrence, Kan: University of Kansas Center for Research, Inc., 1989.

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.