Books on the topic 'Rotori'
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Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. Langley Research Center, 1988.
Find full textRalph, 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. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textWilbur, Matthew L. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textColeman, Colin P. A survey of theoretical and experimental coaxial rotor aerodynamic research. National Aeronautics and Space Administration, 1997.
Find full textCenter, Ames Research, ed. A survey of theoretical and experimental coaxial rotor aerodynamic research. 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. National Aeronautics and Space Administration, Ames Research Center, 1997.
Find full textR, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.
Find full textE, Teske Milton, Quackenbush Todd R, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., and Ames Research Center, eds. A new methodology for free wake analysis using curved vortex elements. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textR, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.
Find full textR, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.
Find full textRunyan, Harry L. Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight. NASA, 1985.
Find full textH, 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. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textPavlović, Momčilo. Rotari klub Subotica: 1929-1941, 1997-2008 = Szabadkai Rotary Klub = Szabadkai Rotary Klub. Rotari klub, 2008.
Find full textMartin, R. M. Acoustic test of a model rotor and tail rotor: Results for the isolated rotors and combined configuration. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textCenter, Ames Research, ed. A study of rotor broadband noise mechanisms and helicopter tail rotor noise. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textRiley, M. J. Measurements of the performance of a helicopter swept tip rotor in flight. [s.n.], 1986.
Find full textRobinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Naval Postgraduate School, 1997.
Find full textInternational 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). Hemisphere Pub. Corp., 1992.
Find full textInternational 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). Hemisphere Pub. Corp., 1992.
Find full textEgolf, T. Alan. A full potential analysis with realistic wake influence for helicopter rotor airload prediction. Ames Research Center, 1987.
Find full textKitaplioglu, Cahit. Analysis of small-scale rotor hover performance data. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textJ, Mack, Mount R, and United States. National Aeronautics and Space Administration., eds. Two rotor stratified charge rotary engine (SCRE) engine system technology evaluation. National Aeronautics and Space Administration, 1994.
Find full textHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Ames Research Center, 1990.
Find full textHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textM, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textM, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: An experimental and analytical investigation of isolated rotor-flap-lag stability in forward flight. Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: Final technical report under NASA-Ames cooperative agreement no. NCC 2-361 (August 1, 1985 - July 31, 1987). Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1987.
Find full textKhánh, Nguyẽ̂n, and Ames Research Center, eds. Aeroelastic stability of a full-scale hingeless rotor. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textKhanh, Nguyen, and Ames Research Center, eds. Aeroelastic stability of a full-scale hingeless rotor. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textKadiĭski, T︠S︡vi︠a︡tko. Rotari v Sofii︠a︡: Legenda i deĭstvitelnost. Kolbis, 2000.
Find full textPeretz, Friedmann, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.
Find full textP, Friedmann Peretz, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.
Find full textChen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textChen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Ames Research Center, 1989.
Find full textCenter, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. National Aeronautics and Space Administration, Ames Research Center, 1993.
Find full textS, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.
Find full textFejtek, Ian G. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Ames Research Center, 1993.
Find full textS, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.
Find full text1936-, Tung C., and Ames Research Center, eds. Performance and pressure data from a small model tilt-rotor in hover. National Aeronautics and Space Administration, Ames Research Center, 1997.
Find full textS, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.
Find full textCenter, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. National Aeronautics and Space Administration, Ames Research Center, 1993.
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