Dynamic response and noise transmission of discretely stiffened composite panels

Mapping Intimacies ◽

10.2514/6.1988-2229 ◽

1988 ◽

Author(s):

CONSTANTINOS LYRINTZIS ◽

RIMAS VAICATIS

Keyword(s):

Dynamic Response ◽

Composite Panels ◽

Stiffened Composite Panels ◽

Noise Transmission

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Random response and noise transmission of discretely stiffened composite panels

Journal of Aircraft ◽

10.2514/3.45915 ◽

1990 ◽

Vol 27 (2) ◽

pp. 176-184 ◽

Author(s):

Constantinos S. Lyrintzis ◽

Rimas Vaicaitis

Keyword(s):

Composite Panels ◽

Random Response ◽

Stiffened Composite Panels ◽

Noise Transmission

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Boundary Collocation Methodology for Stiffened Composite Panels With Large Notch Damage

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-0920 ◽

2021 ◽

Author(s):

Steven G. Russell

Keyword(s):

Composite Panels ◽

Stiffened Composite Panels

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Buckling Reliability Analysis of Stiffened Composite Panels Using an Improved Response Surface Method

Recent Patents on Mechanical Engineering ◽

10.2174/2212797607666140804234100 ◽

2014 ◽

Vol 7 (3) ◽

pp. 247-256

Author(s):

Weitao Zhao ◽

Xiao Li ◽

Feng Guo

Keyword(s):

Reliability Analysis ◽

Response Surface ◽

Response Surface Method ◽

Composite Panels ◽

Surface Method ◽

Stiffened Composite Panels ◽

Improved Response Surface Method

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Damage evolution in fuselage stiffened composite panels under asymmetrical bending loading conditions

10.1063/5.0033945 ◽

2020 ◽

Author(s):

Valerio Acanfora ◽

Andrea Sellitto ◽

Aniello Riccio ◽

Francesco Di Caprio

Keyword(s):

Damage Evolution ◽

Composite Panels ◽

Loading Conditions ◽

Stiffened Composite Panels ◽

Bending Loading ◽

Asymmetrical Bending

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Post-buckling reliability analysis of stiffened composite panels based on adaptive iterative sampling

Engineering With Computers ◽

10.1007/s00366-021-01424-5 ◽

2021 ◽

Author(s):

Feng Zhang ◽

Mingying Wu ◽

Xinting Hou ◽

Cheng Han ◽

Xinhe Wang ◽

...

Keyword(s):

Reliability Analysis ◽

Composite Panels ◽

Stiffened Composite Panels ◽

Iterative Sampling ◽

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Optical measurement on dynamic buckling behavior of stiffened composite panels under in-plane shear

Optics and Lasers in Engineering ◽

10.1016/j.optlaseng.2016.04.017 ◽

2016 ◽

Vol 87 ◽

pp. 111-119 ◽

Author(s):

Zhenkun Lei ◽

Ruixiang Bai ◽

Wang Tao ◽

Xiao Wei ◽

Ruijiao Leng

Keyword(s):

Optical Measurement ◽

Dynamic Buckling ◽

Composite Panels ◽

Plane Shear ◽

Buckling Behavior ◽

Stiffened Composite Panels

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Impact damage detection of curved stiffened composite panels by using wavy embedded small-diameter optical fibers

10.1117/12.475090 ◽

2002 ◽

Author(s):

Hiroaki Tsutsui ◽

Akio Kawamata ◽

Junichi Kimoto ◽

Tomio Sanda ◽

Nobuo Takeda

Keyword(s):

Damage Detection ◽

Optical Fibers ◽

Impact Damage ◽

Small Diameter ◽

Composite Panels ◽

Stiffened Composite Panels

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Effect of elliptical cutouts on buckling and vibration characteristics of stiffened composite panels under non-uniform edge loads

Mechanics Based Design of Structures and Machines ◽

10.1080/15397734.2021.1999266 ◽

2021 ◽

pp. 1-15

Author(s):

Akshay Prakash Kalgutkar ◽

Sauvik Banerjee ◽

T. Rajanna

Keyword(s):

Vibration Characteristics ◽

Composite Panels ◽

Stiffened Composite Panels

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Warping of Stiffened Composite Panels Due to Temperature Changes in the Curing Process

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ◽

10.2514/6.2015-1433 ◽

2015 ◽

Author(s):

Adam Przekop

Keyword(s):

Composite Panels ◽

Curing Process ◽

Temperature Changes ◽

Stiffened Composite Panels

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Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings

Advances in Structural and Multidisciplinary Optimization ◽

10.1007/978-3-319-67988-4_64 ◽

2017 ◽

pp. 838-849

Author(s):

Tobias Bach ◽

Christian Hühne

Keyword(s):

Structural Optimization ◽

Composite Panels ◽

Flexible Aircraft ◽

Aircraft Wings ◽

Stiffened Composite Panels

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