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Method of Rotor Vibration Fault Diagnosis from Process Power Spectrum Entropy and SVM (Unknown language)
- New search for: Fei, C.-w.
- New search for: Bai, G.-c.
- New search for: Li, X.-y.
- New search for: Fei, C.-w.
- New search for: Bai, G.-c.
- New search for: Li, X.-y.
In:
JOURNAL OF PROPULSION TECHNOLOGY -BEIJING-
;
33
, 2
;
293-298
;
2012
-
ISSN:
- Article (Journal) / Print
-
Title:Method of Rotor Vibration Fault Diagnosis from Process Power Spectrum Entropy and SVM
-
Contributors:
-
Published in:JOURNAL OF PROPULSION TECHNOLOGY -BEIJING- ; 33, 2 ; 293-298
-
Publisher:
- New search for: JOURNAL OF PROPULSION TECHNOLOGY
-
Publication date:2012-01-01
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Size:6 pages
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ISSN:
-
Type of media:Article (Journal)
-
Type of material:Print
-
Language:Unknown language
- New search for: 621.4
- Further information on Dewey Decimal Classification
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Classification:
DDC: 621.4 -
Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents – Volume 33, Issue 2
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 167
-
Effect of Total Pressure Distortion on Aerodynamic Stability of CompressorTu, B.-f. / Hu, J. et al. | 2012
- 174
-
Aerodynamic and Heat Transfer of Cooling Blade Tips for High Pressure TurbineYu, K.-h. / Yang, X. / Yue, Z.-f. et al. | 2012
- 179
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Intermediate Turbine Duct Optimization Design Based on One Dimensional Performance ModelYang, J.-g. / Wu, H. / Du, Z.-n. et al. | 2012
- 185
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Quantitative Analysis of Mixing and Combustion in the Scramjet Multi-Cavity CombustorFan, Z.-q. / Liu, W.-d. / Sun, M.-b. et al. | 2012
- 193
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A Model for Simulating the Transient Process for Combustion Chamber of Bipropellant Attitude-Control EngineTang, Z.-y. / Hou, F.-l. / Cai, G.-b. et al. | 2012
- 198
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Bag Breakup of Round Liquid Jets in CrossflowWang, X.-h. / Huang, Y. / Wang, F. et al. | 2012
- 205
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Supersonic Combustion Characteristics of Liquid Kerosene Under Pilot Hydrogen Ignition and Dual-Cavity Flameholding ConditionLi, N. / Song, W.-y. / Luo, F.-t. et al. | 2012
- 211
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Instantaneous Fuel Regression Rate Analysis of Hybrid Rocket Motor ExperimentLi, X.-t. / Zeng, P. / Tian, H. et al. | 2012
- 216
-
Combustion Performance of RBCC Engine with Pylon and Cavity at Ramjet ModePan, K.-w. / He, G.-q. / Qin, f. et al. | 2012
- 221
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Investigation of Mixing Flow Field of Spray Droplets in CrossflowSun, H.-j. / Liu, L. / Zhang, H.-b. et al. | 2012
- 227
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Experiment on Primary Combustion of Pasty Propellant RamjetLiu, A.-h. / Cui, J.-p. / Sun, Z.-h. et al. | 2012
- 232
-
Lean Blow-Out Prediction of Aero-Engine Combustor Based on Cold Flow Field Numerical SimulationHu, B. / Huang, Y. / Wang, F. et al. | 2012
- 239
-
Numerical Study on 3-D Two-Phase Flow of Axisymmetric Shock Induction Controlled Vectoring Exhaust NozzleSong, Y.-f. / Gao, F. / Ma, C.-r. et al. | 2012
- 245
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Experimental Investigation on the Condensed Particles Size Distribution at SRM Nozzle ThroatZhang, S.-m. / Hu, C.-b. / Xia, S.-y. et al. | 2012
- 249
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Exploring on Cooling Effect of Water Injection on Rocket Motor ExhaustZhou, F. / Jiang, Y. / Hao, J.-g. et al. | 2012
- 253
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Film Cooling from a Row of Holes Supplemented with Additional Branched Jet InjectionYang, Y. / Zhang, J.-z. / Yao, Y. et al. | 2012
- 259
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Charring Model of Heat Transfer for Pulse Separation Device of Pulse MotorWang, C.-g. / Tian, W.-p. / Yang, D.-m. et al. | 2012
- 263
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Sensibility Analysis of the Heat Flux in the Rotating CavityDing, S.-t. / Zhang, G. / Li, Y. et al. | 2012
- 269
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Experiments on Heat Transfer Performance Downstream of the Single Cooling Hole in a Flat PlateLiang, J.-Y. / Kang, S. et al. | 2012
- 274
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Numerical Simulation of Coupled Heat Transfer for an Innercooled Blade by Applying Transition k-kl- omega Transition ModelSun, R.-p. / Zhu, W.-b. / Xu, L.-z. et al. | 2012
- 283
-
Combined Model Based Nonlinear Predictive Control for Turboshaft EngineXiao, L.-f. / Zhu, Y. et al. | 2012
- 288
-
Low Cycle Fatigue Probabilistic Life Prediction Models for Fan DiskMu, Y.-w. / Lu, S. et al. | 2012
- 293
-
Method of Rotor Vibration Fault Diagnosis from Process Power Spectrum Entropy and SVMFei, C.-w. / Bai, G.-c. / Li, X.-y. et al. | 2012
- 299
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Investigation on the Effects of Deflector Structure on Detonation Initiation by Shock Wave FocusingRong, K. / He, L.-m. / Zhang, J.-b. et al. | 2012
- 306
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Validation and Performance Analysis for the Quasi-One-Dimensional Models of MHD FlowsChen, R.-f. / Wei, Z.-j. / Wang, N.-f. et al. | 2012
- 313
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Determination of Formation Position for Detonation Wave by Wall Temperature in Pulse Detonation Rocket EngineZhu, X.-d. / Fan, W. / Wang, K. et al. | 2012
- 317
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Experiments on Thrust Measurement of Multi-Cycle Pulse Detonation EngineHe, X.-m. / Li, J.-z. / Wang, J.-h. et al. | 2012
- 322
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Nonlinear Model of Detonation Wave Pressure Based on Ion CurrentPan, M.-x. / Huang, J.-q. et al. | 2012
- 327
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Performance Analysis of Pre-Turbine Hybrid Pulse Detonation EngineQiu, H. / Xiong, C. / Yan, C.-j. et al. | 2012