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Rotors -- Dynamics

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• Rotors
• Dynamics

• Rotors -- Dynamics -- Mathematical models
• Rotors -- Dynamics -- Testing
• Rotors -- Aerodynamics

• Balancing of rigid and flexible rotors (United States Department of Defense, The Shock and Vibration Information Center, 1986), by N. F. Rieger, Naval Research Laboratory (U.S.), and Shock and Vibration Information Center (page images at HathiTrust; US access only)
• Damping in tapered annular seals for an incompressible fluid (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by David P. Fleming, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Off-design performance loss model for radial turbines with pivoting, variable-area stators (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Peter L. Meitner, Arthur J. Glassman, Propulsion Laboratory (U.S.), Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of different rub models on simulated rotor dynamics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Albert F. Kascak, John J. Tomko, United States. Army Aviation Systems Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stability of numerical integration techniques for transient rotor dynamic (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Albert F. Kascak and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance of two-stage fan with larger dampers on first-stage rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Donald C. Urasek, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Coupled rotor/airframe vibration analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Robert Sopher, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United Technologies Corporation. Sikorsky Aircraft Division, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and Langley Research Center (page images at HathiTrust)
• Experiments on multiplane balancing using a laser for material removal (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Russell S. DeMuth, Mechanical Technology Incorporated, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Analytical modeling requirements for tilting proprotor aircraft dynamics (National Aeronautics and Space Administration ;, 1975), by Wayne Johnson, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
• NASA TN D-5506 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Walter Martin Osborn, George W. Lewis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of several porous casing treatments on stall limit and on overall performance of an axial-flow compressor rotor (National Aeronautics and Space Administration ;, 1971), by Walter Martin Osborn, Laurence J. Heidelberg, George W. Lewis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• User's manual : extended capability magnus rotor and ballistic body 6-DOF trajectory program (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by James E. Brunk, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)

• Direct integration of transient rotor dynamics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Albert F. Kascack, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows (NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1990), by A. A. Boretti and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)

• Performance of two-stage fan with a first-state rotor redesigned to account for the presence of a part-span damper (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by William T. Gorrell, Donald C. Urasek, Propulsion Laboratory (U.S.), Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• NASA TN D-4537 (National Aeronautics and Space Administration ;, 1968), by Alan D. Levin, Ronald C. Smith, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Laser anemometer measurements in a transonic axial-flow fan rotor (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Anthony J. Strazisar and Lewis Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• ARF project no. K206, final report. Development of methods and equipment for balancing flexible rotors. Issued May 1962 for Bureau of Ships, Dept. of the Navy, under contract no. NObs-78753. ([Washington, 1963), by IIT Research Institute and United States Navy Department Bureau of Ships (page images at HathiTrust)
• Certain brake drums and rotors from China (U.S. International Trade Commission, 1996), by United States International Trade Commission (page images at HathiTrust)
• Certain brake drums and rotors from China (U.S. International Trade Commission, 1997), by United States International Trade Commission (page images at HathiTrust)
• Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Susan L. Althoff and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• In-place recalibration technique applied to a capacitance-type system for measuring rotor blade clearance (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by John P. Barranger and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Jeffrey E. Haas, Milton G. Kofskey, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effects of geometric variables on rub characteristics of Ti-6A1-4V (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Robert C. Bill, Donald W. Wisander, Jan Wolak, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lewis Research Center, and Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Incidence loss for fan turbine rotor blade in two-dimensional cascade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by John F. Kline, Roy G. Stabe, Thomas P. Moffitt, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows (NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1990), by A. A. Boretti and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Experimental investigation of advanced concepts to increase turbine blade loading. III, Performance evaluation of tandem rotor blade (National Aeronautics and Space Administration ;, 1968), by H. G. Lueders, General Motors Corporation. Allison Division, and Lewis Research Center (page images at HathiTrust)
• Performance comparisons of high mach number compressor rotor blading (National Aeronautics and Space Administration ;, 1968), by J. P. Gostelow, L. H. Smith, K. W. Krabacher, Lewis Research Center, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heliogyro solar sailer : summary report (National Aeronautics and Space Administration ;, 1969), by Richard H. MacNeal, Hans U. Schuerech, John M. Hedgepeth, United States National Aeronautics and Space Administration, and Astro Research Corporation (page images at HathiTrust)
• Effects of vibration and shock on the performance of gas-bearing space power Brayton cycle turbomachinery. I, Half-sine shock and sinusoidal vibration (National Aeronautics and Space Administration ;, 1971), by Paul R. Spencer, Henry B. Tryon, Peter W. Curwen, and Mechanical Technology Incorporated (page images at HathiTrust)
• Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 1, Model and results (National Aeronautics and Space Administration ;, 1971), by S. G. Sadler, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 2, Program listings (National Aeronautics and Space Administration ;, 1971), by S. G. Sadler, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Flexible rotor balancing by the influence coefficient method : multiple critical speeds with rigid or flexible supports (National Aeronautics and Space Administration ;, 1975), by Juergen M. Tessarzik, Lewis Research Center, and Mechanical Technology Incorporated (page images at HathiTrust)
• Nonlinear actuator disk theory and flow field calculations, including nonuniform loading (National Aeronautics and Space Administration ;, 1970), by Michael D. Greenberg, Stephen R. Powers, Langley Research Center, and Inc Sage Action (page images at HathiTrust)
• Balancing techniques for high-speed flexible rotors (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by A. J. Smalley, R. A. Rio, J. M. Tessarzik, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Design and experimental results for a turbine with jet flap stator and jet flap (National Aeronautics and Space Administration ;, 1973), by James L. Bettner, Jerry O. Blessing, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Foil bearings for axial and radial support of high speed rotors : design, development, and determination of operating characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Lazar Licht and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• NASA TR R-71 (National Aeronautics and Space Administration ;, 1960), by Harry H. Heyson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Reliability approach to rotating-component design (National Aeronautics and Space Administration ;, 1975), by Dimitri Kececioglu, Vincent R. Lalli, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-2481 (National Aeronautics and Space Administration :, 1964), by James E. Crouse, Donald M. Sandercock, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5256 (National Aeronautics and Space Administration ;, 1969), by Robert J. Huston, James P. Shivers, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4065 (National Aeronautics and Space Administration ;, 1967), by Ronald C. Smith, Alan D. Levin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of four inlet and outlet tip-annulus-area blockage configurations on the performance of an axial-flow fan rotor (National Aeronautics and Space Administration ;, 1976), by Walter Martin Osborn, Roy D. Hager, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5602 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Julian L. Jenkins, Perry L. Deal, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground effect for lifting rotors in forward flight (National Aeronautics and Space Administration, 1960), by Harry H. Heyson and Langley Research Center (page images at HathiTrust)
• Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid (National Aeronautics and Space Administration, 1959), by George C. Ashby and Langley Research Center (page images at HathiTrust)
• Correlation of part-span damper losses through transonic rotors operating near design point (National Aeronautics and Space Administration ;, 1977), by William B. Roberts and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Behavior of a rotor in a two-phase field (1901), by O.L. Housel (page images at HathiTrust; US access only)
• Construction and test of a slip meter (1908), by Clarence Benwell Miller and George Richard Welch (page images at HathiTrust; US access only)
• Stability of an aerodynamic body with a rotor (Sandia Corporation ;, 1957), by Frederick Gwynn Blottner, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Low speed rotary motors for sealed systems (Washington, D.C. : Office of Technical Services, Department of Commerce, 1954., 1954), by W. E. McCown, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation. Atomic Power Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Distributed generation drivetrain for high torque wind turbine applications : final project report (California Energy Commission, 2011), by Amir Mikhail, Clipper Windpower Technology Inc, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)
• Development of an oscillating vane concept as an innovative wind energy conversion system (Solar Energy Research Institute ;, 1982), by Richard L Bielawa, United Technologies Research Center, United States. Department of Energy, and Solar Energy Research Institute (page images at HathiTrust)
• Reduction of the 4th-order asymmetric-rotor Hamiltonian (L. G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1966., 1966), by F. X. Kneizys, S. A. Clough, J. N. Freedman, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)

More items available under broader and related terms at left.