The General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure

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ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure by : John N. Dickson

Download or read book The General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure written by John N. Dickson and published by . This book was released on 1969 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the General Instability of Ring-stiffened Cylindrical Shells Under the Action of Radial External Pressure and Axial Compression

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ISBN 13 :
Total Pages : 126 pages
Book Rating : 4.:/5 (154 download)

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Book Synopsis On the General Instability of Ring-stiffened Cylindrical Shells Under the Action of Radial External Pressure and Axial Compression by : Sesto Joseph Voce

Download or read book On the General Instability of Ring-stiffened Cylindrical Shells Under the Action of Radial External Pressure and Axial Compression written by Sesto Joseph Voce and published by . This book was released on 1965 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression

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ISBN 13 :
Total Pages : 55 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis On the Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression by : Josef Singer

Download or read book On the Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression written by Josef Singer and published by . This book was released on 1965 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt: The eccentricity effect of stiffeners is studied for stiffened cylindrical shells under axial compression. Classical simple supports and classical clamped ends are considered. A detailed physical explanation of the causes of the eccentricity effect and its behavior is proposed and verified by computations for 350 typical shells. As for buckling under hydrostatic pressure and torsion studied earlier, the behavior of the eccentricity effect in the case of axial compression also depends very strongly on the geometry of the shell, represented by the Batdorf parameter, while the geometry of the stiffeners only influences its magnitude. Inversion of eccentricity effect occurs at very low Z, but for practical dimensions outside stringers always stiffen the shell more than inside ones. The eccentricity effect has a pronounced maximum at practical values of Z, and the behavior of the eccentricity effect is very similar for clamped and simply supported shells. Rings, which are much less effective stiffeners than stringers under axial compression, are also considered. Results are compared with those of other investigators. (Author).

Buckling of Stiffened Cylinders in Axial Compression and Bending

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Buckling of Stiffened Cylinders in Axial Compression and Bending by : James P. Peterson

Download or read book Buckling of Stiffened Cylinders in Axial Compression and Bending written by James P. Peterson and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Buckling data review for stiffened cylinder failures during axial compression and bending.

The Stability Under Axial Compression and Lateral Pressure of Circular-cylindrical Shells with a Soft Elastic Core

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ISBN 13 :
Total Pages : 57 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis The Stability Under Axial Compression and Lateral Pressure of Circular-cylindrical Shells with a Soft Elastic Core by : Paul Seide

Download or read book The Stability Under Axial Compression and Lateral Pressure of Circular-cylindrical Shells with a Soft Elastic Core written by Paul Seide and published by . This book was released on 1961 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: The stability under axial compression and lateral pressure of a finite circular-cylindrical shell with an elastic core is treated by means of Donnell's equations. The stability criterion is investigated in detail for the general cylinder under axial compression or lateral pressure and for a particular cylinder under combined loading. Comparisons are made with available experimental data. (Author).

NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 966 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Linear Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression

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ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Linear Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression by : Tien-Yu Tsui

Download or read book Linear Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression written by Tien-Yu Tsui and published by . This book was released on 1973 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linear stability of eccentrically stiffened cylindrical shells under axial compression has been investigated in the paper with an aim to establish the parameter ranges for the prevailing buckling modes. Charts delineating the zones of prevailing modes are presented in a parameter plane. Useful approximate relations are given for the bounds on parameters to predict a buckling mode for a shell in the moderate length range. (Author).

NASA Technical Note

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ISBN 13 :
Total Pages : 332 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The General Instability of Stiffened Cylindrical Shells Under Axial Compression

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (632 download)

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Book Synopsis The General Instability of Stiffened Cylindrical Shells Under Axial Compression by : Arie van der Neut

Download or read book The General Instability of Stiffened Cylindrical Shells Under Axial Compression written by Arie van der Neut and published by . This book was released on 1947 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Computerized buckling analysis of shells

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Publisher : Springer Science & Business Media
ISBN 13 : 9789024730995
Total Pages : 456 pages
Book Rating : 4.7/5 (39 download)

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Book Synopsis Computerized buckling analysis of shells by : D. Bushnell

Download or read book Computerized buckling analysis of shells written by D. Bushnell and published by Springer Science & Business Media. This book was released on 1985-09-30 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 722 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1979 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing

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ISBN 13 :
Total Pages : 956 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Collected Papers on Instability of Shell Structures, 1962

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ISBN 13 :
Total Pages : 800 pages
Book Rating : 4.X/5 (1 download)

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Book Synopsis Collected Papers on Instability of Shell Structures, 1962 by : NASA Symposium on Instability of Shell Structures

Download or read book Collected Papers on Instability of Shell Structures, 1962 written by NASA Symposium on Instability of Shell Structures and published by . This book was released on 1962 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Buckling of Thin Metal Shells

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Publisher : CRC Press
ISBN 13 : 1482295075
Total Pages : 518 pages
Book Rating : 4.4/5 (822 download)

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Book Synopsis Buckling of Thin Metal Shells by : J.G. Teng

Download or read book Buckling of Thin Metal Shells written by J.G. Teng and published by CRC Press. This book was released on 2006-06-28 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thin-walled metal shell structures are highly efficient in their use of material, but they are particularly sensitive to failure by buckiling. Many different forms of buckling can occur for different geometries and different loading conditions. Because this field of knowledge is both complex and industrially important, it is of great interest and c

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 912 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : pages
Book Rating : 4.3/5 (121 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells Under Torsion

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells Under Torsion by : Manahem Baruch

Download or read book Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells Under Torsion written by Manahem Baruch and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method of analysis of eccentrically stiffened cylindrical shells, developed earlier, is applied to buckling under torsion. In the calculations about 350 shells covering a wide range of shell and stiffener geometries have been considered. It is found that for long cylinders rings are the important stiffeners, and internal rings stiffen more than external rings. For short cylinders the effect is inverted, external rings yielding higher critical loads than internal rings. Stringers have little effect in long cylinders, but in short cylinders they stiffen the shell against buckling in torsion as much as rings. Outside stringers always stiffen the shell more than inside stringers. (Author).