Wing instability of a full composite aircraft-Reference-Cited by-同舟云学术

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Wing instability of a full composite aircraft

Published:2001-11 Issue:2-3 Volume:54 Page:335-340
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Shokrieh Mahmood M.,Taheri Behrooz Fathollah

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference10 articles.

1. Scanian RH, Rosenbaum R. Aircraft vibration and flutter; 1996

2. Principles of aeroelasticity;Bisplinghoff,1989

3. JAR-23, Joint aviation requirements, 11 March 1994

4. Nisa II/display III user manual, vol. 2; 1992

5. Zienkiewicz OC, Taylor RL. The finite element method. 4th ed., vol. I; 1989

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1. Vibration Analysis and Active Control of Irregular Integrated Composite Sandwich Plates with Incompletely Constrained Boundaries;2024

2. Promising Wing Vibration Measurement System Using MEMS IMUS and Kalman Filter Correction;International Journal of Applied Mechanics and Engineering;2022-06-01

3. Flutter analysis of a sandwich composite beam using an analytical method;Journal of Sandwich Structures & Materials;2020-09-01

4. Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio;International Journal of Aerospace Engineering;2019-07-11

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