3 edition of Free vibrations of thin-walled semicircular graphite-epoxy composites found in the catalog.
Free vibrations of thin-walled semicircular graphite-epoxy composites
by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, National Technical Information Service, distributor] in [Washington, DC], [Springfield, Va
Written in English
|Other titles||Free vibrations of thin walled semicircular graphite-epoxy composites.|
|Statement||Ahmed K. Noor, Huey D. Carden, Jeanne M. Peters.|
|Series||NASA technical paper -- 3010.|
|Contributions||Carden, Huey D., Peters, Jeanne M., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.|
|The Physical Object|
Haim Abramovich (Editor), Stability and Vibrations of Thin-Walled Composite Structures, Woodhead Publishing, June , pages. Satya N. Atluri, Sam G. Sampath and Pin Tong (Editors), Structural Integrity of Aging Airplanes, Springer, , pages. Free vibrations of thin-walled semicircular graphite-epoxy composite frames / (Washington, D.C.: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va.
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Finite Elements in Analysis and Design 9 () 33 Elsevier Free vibrations of thin-walled semicircular graphite-epoxy composite frames Ahmed K. Noor 1, Huey D. Carden and Jeanne M. Peters 1 NASA Langley Research Center, Hampton, VAUSA Received May Revised November by: 7. NASA Technical Memorandum Free Vibrations of Thin-Walled Semicircular Graphite-Epoxy Composite Frames Huey D.
Carden, Ahmed K. Noor, and Jeanne M. Peters. Free vibrations of thin-walled semicircular graphite-epoxy composite frames. Author links open overlay panel Ahmed N. Noor 1 Huey D. Carden Jeanne M. Peters 1Cited by: 7. Get this from a library. Free vibrations of thin-walled semicircular graphite-epoxy composites.
[Ahmed Khairy Noor; Huey D Carden; Jeanne M Peters; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.]. Get this from a library.
Free vibrations of thin-walled semicircular graphite epoxy composite frames. [Huey D Carden; Ahmed Khairy Noor; Jeanne M Peters; Langley Research Center.]. Free vibrations of thin-walled semicircular graphite-epoxy composite frames.
A detailed study is made of the effects of variations in lamination and material parameters of thin walled composite frames on their vibrational characteristics. The structures considered are semicircular thin walled frames with I and J sections.
The flanges and. Free vibrations of thin-walled semicircular graphite-epoxy composite frames / By Ahmed Khairy Noor, Jeanne M. Peters, Huey D. Carden and Langley Research Center. Abstract. Numerical and experimental investigation of the collapse response of thin-walled graphite-epoxy cylindrical shells loaded in bending.
On the free vibrations of a thin-walled cylindrical shell subjected to a bending moment (Effect of bending moment on free vibrations of thin walled cylindrical shell, using modified donnell equation and by: 8. Experiments were conducted to measure the 3-D static and free vibrational response of two graphite-epoxy, thin walled, open section frames.
The. Stability and Vibrations of Thin-Walled Composite Structures presents engineering and academic knowledge on the stability (buckling and post buckling) and vibrations of thin walled composite structures like columns, plates, and stringer stiffened plates and shells, which form the basic structures of the aeronautical and space sectors.
Currently, this knowledge is dispersed in several books. Numerical results are presented for semicircular thin-walled frames with I and J section, showing the convergence of the nonlinear frequency and the sensitivity coefficients obtained by both the. The Schrödinger equation for a free particle which is restricted to a semicircle (technically, whose configuration space is the circle) is Free vibrations of thin-walled semicircular graphite-epoxy composite frames.
Abstract A detailed study is made of the effects of variations in lamination and material parameters of thin-walled. Free vibrations of thin-walled semicircular graphite-epoxy composite frames Finite Elements in Analysis and Design, Vol. 9, No. 1 Thin-walled composite beams under bending, torsional, and extensional loadsCited by: Free vibration of fully functionally graded carbon nanotube reinforced graphite/epoxy laminates Kuo S Y and Shiau L C Buckling and vibration of composite laminated plates with variable fiber spacing Compos.
Struct Kuo S Y Vibration of thermally post-buckled hybrid laminates with two non-uniformly distributed fibers Thin-Walled Cited by: 3. This paper evaluates the vibration characteristics of thin/thick rotating cylindrical shells made of metallic and composite materials.
A previous theory of the authors is extended here to include the effects of geometrical stiffness due to by: A thermal environment has a complex influence on the dynamic characteristics of fiber-reinforced composite materials and structures.
It is challenging to consider the effects of high temperature and external vibration energy simultaneously on their nonlinear vibration response. In this research, the material nonlinearities, due to both the excitation amplitudes and the high. Loos, A.C.
and Springer, G.S., “Curing of Graphite/Epoxy Composites”, Air Force Materials Laboratory Report AFWAL-TR– Wright Aeronautical Laboratories, Wright Patterson Air Force Base, Dayton, OH. Google ScholarCited by: graphite/epoxy composites. These materials have been used to meet a wide variety of design param eters ranging from minimal weight to high struc tural stiffness requirements.
Because of their ability to meet many diverse design requirements simulta neously the use of graphite/epoxy composites is expected to by: 1. Murugan R, Padmanabhan K, Ramesh R, “Vibration Characteristics of Thin Walled Hybrid Carbon Composite Beams under Fixed Free Boundary Condition” in 3rd Asian Conference on Mechanics of Functional Materials and Structures (ACMFMS ) held on Decemberat Indian Institute of Technology, New Delhi 3.
Free vibration (or eigenvalue analysis) is a prerequisite for aeroelastic analysis. For divergence analysis, slope influence coefficients (rotation at point i due to unit load at point j) are calculated using free vibration mode shapes and corresponding frequencies.
The lowest eigenvalue is of interest and gives the divergence speed. The present paper considers the maximization Cited by: 5. A random short-fiber composite is shown in Fig. Fiber-reinforced composites are widely used in thin-walled aircraft structures because of their specific high strength.
For example, the graphite-epoxy composite is characterized by a unidirectional tensile strength of GPa while the density is Mg/rrt?.This paper aims to provide an overview of engineering analysis methods concerning the buckling and post-buckling behavior of thin-walled composite laminated beams, covering topics such as exact and closed-form analytical approximate solutions as well as semi-analytical and numerical methods wherein a distinction is made between local and global Author: Christian Mittelstedt.Song, O.
and Librescu, L. () “Free Vibration of Anisotropic Composite Thin-Walled Beams of Closed Cross-Section Contour,” Journal of Sound and Vibration, Vol.No. 1, pp. – CrossRef Google Scholar.