Książki na temat „Rotors”

Ralph, Jolly J., Marcolini Michael A i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

Bachschmid, Nicolò, Paolo Pennacchi i Ezio Tanzi. Cracked Rotors. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-01485-7.

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

Wilbur, Matthew L. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Center, Langley Research, red. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Center, Langley Research, red. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Center, Langley Research, red. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Center, Langley Research, red. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Ganguli, Ranjan, Dipali Thakkar i Sathyamangalam Ramanarayanan Viswamurthy. Smart Helicopter Rotors. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-24768-7.

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

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

H, Tai, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.

Center, Ames Research, red. 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, red. 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.

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.

Riley, M. J. Measurements of the performance of a helicopter swept tip rotor in flight. [S.l.]: [s.n.], 1986.

Lee, Chong-Won. Vibration Analysis of Rotors. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8173-8.

Ghandehari, Mostafa. Self-circumference of rotors. Arlington: Dept. of Mathematics, University of Texas at Arlington, 1996.

Lee, Chong-Won. Vibration Analysis of Rotors. Dordrecht: Springer Netherlands, 1993.

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

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--dynamics: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--transport phenomena: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.

Krämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-662-02798-1.

Vullo, Vincenzo, i Francesco Vivio. Rotors: Stress Analysis and Design. Milano: Springer Milan, 2013. http://dx.doi.org/10.1007/978-88-470-2562-2.

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

Vullo, Vincenzo. Rotors: Stress Analysis and Design. Milano: Springer Milan, 2013.

Center, Ames Research, red. Soft hub for bearingless rotors. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

Krämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993.

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.

R, Johnson Wayne, i United States. National Aeronautics and Space Administration., red. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.

R, Johnson Wayne, i United States. National Aeronautics and Space Administration., red. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.

E, Teske Milton, Quackenbush Todd R, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. i Ames Research Center, red. A new methodology for free wake analysis using curved vortex elements. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

R, Johnson Wayne, i United States. National Aeronautics and Space Administration., red. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.

Paxson, Daniel E. An improved numerical model for wave rotor design and analysis. [Washington, DC: National Aeronautics and Space Administration, 1992.

Chattopadhyay, Aditi. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.

Martin, R. M. Wind-tunnel acoustic results of two rotor models with several tip designs. Hampton, Va: Langley Research Center, 1986.

Corrigan, Robert D. Performance and power regulation characteristics of two aileron-controlled rotors and a pitchable tip-controlled rotor on the Mod-O wind turbine. Washington, DC: U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division, 1987.

A, Silva Walter, i Langley Research Center, red. The effects of aeroelastic deformation on the unaugmented stopped-rotor dynamics of an x-wing aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

United States. National Aeronautics and Space Administration., red. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.

Rieger, N. F. Balancing of rigid and flexible rotors. Washington, DC: Shock and Vibration Information Center, U.S. Dept. of Defense, 1986.

Rosenstein, H. Aerodynamic development of the V-22 tilt rotor. [S.l.]: [s.n.], 1986.

Rosenstein, H. Aerodynamic development of the V-22 tilt rotor. New York: AIAA, 1986.

Sergeev, S. V. Vibrat︠s︡ionnye rotornye privody mashin. Cheli︠a︡binsk: I︠U︡zhno-Uralʹskiĭ gos. universitet, 2007.

Paolo, Pennacchi Ezio Tanzi Nicol Bachschmid. Cracked Rotors. Springer, 2010.

Gilliand, Jr. Dancing Rotors. Midland Publishing, 1996.