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Books on the topic 'Turbine blade vibration'

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Author: Grafiati
Published: 14 March 2023

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1

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

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2

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

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3

M, Greitzer Edward, George C. Marshall Space Flight Center., and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

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4

M, Greitzer Edward, George C. Marshall Space Flight Center, and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

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5

R, Little Ronald, and United States. National Aeronautics and Space Administration, eds. Application of a personal computer for the uncoupled vibration analysis of wind turbine blade and counterweight assemblies. [Washington, DC: National Aeronautics and Space Administration, 1985.

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6

V, Nagpal, Chamis C. C, and United States. National Aeronautics and Space Administration., eds. Probabilistic analysis of bladed turbine disks and the effect of mistuning. [Washington, D.C: National Aeronautics and Space Administration, 1990.

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7

1959-, Pierre Christophe, and United States. National Aeronautics and Space Administration., eds. Stochastic sensitivity measure for mistuned high-performance turbines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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8

Center, Lewis Research, ed. Effects of mistuning and matrix structure on the topology of frequency response curves. Cleveland, Ohio: Lewis Research Center, 1989.

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9

Afolabi, Dare. Effects of mistuning and matrix structure on the topology of frequency response curves. Cleveland, Ohio: Lewis Research Center, 1989.

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10

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Programmer's manual. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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11

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Theoretical manual. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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12

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): User's manual. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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13

M-T, Yang, and United States. National Aeronautics and Space Administration., eds. Modeling the effect of shroud contact and friction dampers on the mistuned response of turbopumps: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

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14

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Interim report. [Cleveland, Ohio]: National Aeronautics and Space Administration, 1988.

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15

M-T, Yang, and United States. National Aeronautics and Space Administration., eds. Modeling the effect of shroud contact and friction dampers on the mistuned response of turbopumps. [Washington, DC: National Aeronautics and Space Administration, 1994.

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16

A, Hopkins Dale, and Lewis Research Center, eds. Thermoviscoplastic nonlinear constitutive relationships for structural analysis of high temperature metal matrix composites. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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17

Raczynski, Adam. Gas turbine blade vibration: Influencing factors and their effects. LAP Lambert Academic Publishing, 2010.

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