Combination Resonance Instability of Curved Panels with Cutout Subjected to Nonuniform Loading with Damping-Reference-Cited by-同舟云学术

Combination Resonance Instability of Curved Panels with Cutout Subjected to Nonuniform Loading with Damping

Published:2008-07 Issue:7 Volume:134 Page:555-566
ISSN:0733-9399
Container-title:Journal of Engineering Mechanics
language:en
Short-container-title:J. Eng. Mech.

Author:

Udar Ratnakar. S.¹²,Datta P. K.¹²

Affiliation:

1. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721302, India. E-mail: sanjaysu1114@yahoo.co.in

2. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721302, India (corresponding author). E-mail: pkdatta@aero.iitkgp.ernet.in

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290733-9399%282008%29134%3A7%28555%29

Reference44 articles.

1. Dynamic stability of a composite circular cylindrical shell subjected to combined axial and torsional loading;Argento A.;J. Compos. Mater.,1993

2. Stability characteristics of composite panels with various cutout geometries

3. Effect of damping on the postcritical behaviour of autonomous non-conservative systems

4. Dynamic behavior of a cylinder with a cutout.

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