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Journal Articles

Specific Features of Dynamic Behavior of Stationary and Rotating Single/Coaxial Cylindrical Shells Interacting With the Axial and Rotational Fluid Flows

Sergey A. Bochkarev, Valery P. Matveenko
Journal: Journal of Vibration and Acoustics
Publisher: ASME
Article Type: Research-Article
J. Vib. Acoust. April 2015, 137(2): 021001.
Paper No: VIB-13-1176
https://doi.org/10.1115/1.4028829
Published Online: April 1, 2015
... [36] Cortelezzi , L. , Pong , A. , and Païdoussis , M. P. , 2004 , “ Flutter of Rotating Shells With a Co-Rotating Axial Flow ,” ASME J. Appl. Mech. , 71 ( 1 ), pp. 143 – 145 . 10.1115/1.1636794 [37] Bochkarev , S. A. , and Matveenko , V. P. , 2013 , “ Numerical...
View Article titled, Specific Features of Dynamic Behavior of Stationary and Rotating Single/Coaxial Cylindrical Shells Interacting With the Axial and Rotational Fluid Flows
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Topics: Fluids, Shells, Stability, Fluid dynamics, Pipes, Flow (Dynamics)
Journal Articles

Fuzzy Approximation by a Novel Levenberg–Marquardt Method for Two-Degree-of-Freedom Hypersonic Flutter Model

Y. H. Wang, L. Zhu, Q. X. Wu, C. S. Jiang
Journal: Journal of Vibration and Acoustics
Publisher: ASME
Article Type: Technical Briefs
J. Vib. Acoust. August 2014, 136(4): 044502.
Paper No: VIB-13-1103
https://doi.org/10.1115/1.4027524
Published Online: May 19, 2014
... ) approximation error of f 3 ( x ), ( c ) fuzzy approximation of f 4 ( x ), and ( d ) approximation error of f 4 ( x ). A more precise mathematical model will provide more effective help for the suppression of hypersonic flutter. In this paper, an online fuzzy modeling scheme without any human...
View Article titled, Fuzzy Approximation by a Novel Levenberg–Marquardt Method for Two-Degree-of-Freedom Hypersonic <span class="search-highlight">Flutter</span> Model
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Topics: Airfoils, Approximation, Flutter (Aerodynamics), Errors
Journal Articles

Efficient Hybrid Finite Element Method for Flutter Prediction of Functionally Graded Cylindrical Shells

Farhad Sabri, Aouni A. Lakis
Journal: Journal of Vibration and Acoustics
Publisher: ASME
Article Type: Research-Article
J. Vib. Acoust. February 2014, 136(1): 011002.
Paper No: VIB-10-1286
https://doi.org/10.1115/1.4025397
Published Online: September 27, 2013
... AND A COUSTICS . Manuscript received December 2, 2010; final manuscript received July 15, 2013; published online September 27, 2013. Assoc. Editor: Bogdan Epureanu. 02 12 2010 15 07 2013 In this work, a hybrid finite element formulation is presented to predict the flutter boundaries...
View Article titled, Efficient Hybrid Finite Element Method for <span class="search-highlight">Flutter</span> Prediction of Functionally Graded Cylindrical Shells
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Topics: Finite element methods, Flutter (Aerodynamics), Pipes, Shells, Stiffness, Pressure, Materials properties, Ceramics, Functionally graded materials, Modeling
Journal Articles

Panel Flutter Model Identification Using the Minimum Model Error Method on the Forced Response Measurements

Oleg V. Shiryayev, Joseph C. Slater
Journal: Journal of Vibration and Acoustics
Publisher: ASME
Article Type: Technical Papers
J. Vib. Acoust. October 2006, 128(5): 635–645.
https://doi.org/10.1115/1.2202160
Published Online: February 8, 2006
...Oleg V. Shiryayev; Joseph C. Slater This work illustrates application of the minimum model error system identification method to obtain the nonlinear state space models of a fluttering panel. Identification using position and velocity data from forced response of the panel is presented here...
View Article titled, Panel <span class="search-highlight">Flutter</span> Model Identification Using the Minimum Model Error Method on the Forced Response Measurements
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Topics: Errors, Flow (Dynamics), Flutter (Aerodynamics), Transients (Dynamics), Noise (Sound), Response surface methodology, System identification, Eigenvalues, Algorithms, Simulation