Books on the topic 'Rotors – Aerodynamics'
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Coleman, Colin P. A survey of theoretical and experimental coaxial rotor aerodynamic research. Washington, D.C: National Aeronautics and Space Administration, 1997.
Find full textAerodynamics of wind turbines: Rotors, loads and structure. London: James X James [i.e. James & James], 2000.
Find full textCross, 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.
Find full textBeesten, Benno. Nichtplanare Rotorblattspitzen im Hubschraubervorwärtsflug. Göttingen: Cuvillier, 1996.
Find full textAlthoff, 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.
Find full textKroll, Norbert. Berechnung von Strömungsfeldern um Propeller und Rotoren im Schwebeflug durch die Lösung der Euler-Gleichungen. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1989.
Find full textRoberts, Thomas W. Euler equation computations for the flow over a hovering helicopter rotor. [Washington, DC]: National Aeronautics and Space Administration, 1988.
Find full textRutherford, 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.
Find full textKitaplioglu, Cahit. Analysis of small-scale rotor hover performance data. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textMihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textKolokolov, S. N. Dinamika upravli͡a︡emogo dvizhenii͡a︡ vertoleta. Moskva: "Mashinostroenie", 1987.
Find full textKunz, 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.
Find full textMihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textKunz, 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.
Find full textMihaloew, James R. Rotorcraft flight-propulsion control integration: An eclectic design concept. Cleveland, Ohio: Lewis Research Center, 1988.
Find full textChattopadhyay, Aditi. Performance of an optimized rotor blade at off-design flight conditions. Washington, DC: National Aeronautics and Space Administration, 1990.
Find full textBerry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.
Find full textBerry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.
Find full textBerry, John D. Flapping inertia for selected rotor blades. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textBerry, John D. RWF rotor-wake-fuselage code software reference guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Cneter, 1991.
Find full textMurthy, V. R. Comprehensive analysis of helicopters with bearingless rotors: Status report. Syracuse, N.Y: Syracuse University, Dept. of Mechanical and Aerospace Engineering, 1988.
Find full textHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.
Find full textHamade, 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.
Find full textRostafiński, Wojciech. Analysis of fully stalled compressor. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textBerry, 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.
Find full textNorman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textNorman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textNorman, Tom. Application of the wide-field shadowgraph technique to rotor wake visualization. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textPaxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textPaxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textLance, 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.
Find full textLance, 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.
Find full textMineck, 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.
Find full textCenter, 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.
Find full textUnited 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.
Find full textCenter, 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.
Find full textCenter, 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.
Find full textCenter, Ames Research, ed. Tilt rotor hover aeroacoustics. [Moffett Field, Calif.]: National Aeronautics and Space Administration, Ames Research Center, 1992.
Find full textAerodynamic parameter studies and sensitivity analysis for rotor blades in axial flight. Hampton, Va: Lockheed Engineering & Science Co., 1991.
Find full textCenter, 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.
Find full textSheng, Chunhua. Advances in Transitional Flow Modeling: Applications to Helicopter Rotors. Springer London, Limited, 2016.
Find full textWang, Jingyu, and Chunhua Sheng. Advances in Transitional Flow Modeling: Applications to Helicopter Rotors. Springer International Publishing AG, 2016.
Find full textPatrick, 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.
Find full text1936-, 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.
Find full text1936-, 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.
Find full textCenter, 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.
Find full textW, 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.
Find full text1936-, 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.
Find full textCooperative 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.
Find full text1936-, 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.
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