Interior aircraft noise computations due to TBL excitation using the energy finite element analysis

[1]  Nickolas Vlahopoulos,et al.  An energy finite element formulation for high-frequency vibration analysis of externally fluid-loaded cylindrical shells with periodic circumferential stiffeners subjected to axi-symmetric excitation , 2005 .

[2]  Nickolas Vlahopoulos,et al.  Numerical Implementation, Validation, and Marine Applications of an Energy Finite Element Formulation , 1999 .

[3]  Aimin Wang,et al.  High-frequency vibration analysis of thin elastic plates under heavy fluid loading by an energy finite element formulation , 2003 .

[4]  Application of energy finite elements in the prediction of the vibroacoustic ground response of business jet , 2008 .

[5]  Aimin Wang,et al.  An alternative energy finite element formulation based on incoherent orthogonal waves and its validation for marine structures , 2002 .

[6]  Geng Zhang,et al.  Validation of an EFEA formulation for computing the vibrational response of complex structures , 2007 .

[7]  Xiaoyan Yan Energy Finite Element Analysis Developments for High Frequency Vibration Analysis of Composite Structures. , 2008 .

[8]  Aimin Wang,et al.  Energy finite element analysis of the NASA aluminum testbed cylinder , 2005 .

[9]  S. Hambric,et al.  Comparison of semi-empirical models for turbulent boundary layer wall pressure spectra , 2009 .

[10]  Yvan Champoux,et al.  New empirical equations for sound propagation in rigid frame fibrous materials , 1992 .

[11]  Aimin Wang,et al.  A vibration analysis of stiffened plates under heavy fluid loading by an energy finite element analysis formulation , 2005 .

[12]  Nickolas Vlahopoulos,et al.  A Substructuring Formulation for the Energy Finite Element Analysis , 2007 .

[13]  Nick Vlahopoulos,et al.  An EFEA Formulation for Computing Structural Response of Complex Structures , 2005 .

[14]  Aimin Wang,et al.  Parametric design sensitivity analysis of high-frequency structural-acoustic problems using energy finite element method , 2005 .

[15]  J. E. Robertson,et al.  Vibration response of spacecraft shrouds toin-flight fluctuating pressures , 1974 .