The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression

The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression PDF Author: John N. Dickson
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ISBN:
Category : Axial flow compressors
Languages : en
Pages : 44

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A method is presented to determine the general instability load of a ring-stiffened corrugated cylinder under axial compression. This method is developed using linear small deflection theory. The stiffness properties of the rings are uniformly distributed along the cylinder and the eccentricity of the rings with respect to the corrugation centerline is taken into account. Analytical and experimental results are compared. In this comparison good agreement is obtained for cylinders loaded in pure compression. For the cylinders subjected to bending or a combination of bending and compression the analytical calculations are conservative. A computer program for the application of this method has been developed. The program and an explanation of its notation are included in this report.

The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression

The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression PDF Author: John N. Dickson
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 44

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Book Description
A method is presented to determine the general instability load of a ring-stiffened corrugated cylinder under axial compression. This method is developed using linear small deflection theory. The stiffness properties of the rings are uniformly distributed along the cylinder and the eccentricity of the rings with respect to the corrugation centerline is taken into account. Analytical and experimental results are compared. In this comparison good agreement is obtained for cylinders loaded in pure compression. For the cylinders subjected to bending or a combination of bending and compression the analytical calculations are conservative. A computer program for the application of this method has been developed. The program and an explanation of its notation are included in this report.

NASA Technical Note

NASA Technical Note PDF Author:
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Category : Aeronautics
Languages : en
Pages : 814

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

The General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure PDF Author: John N. Dickson
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ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124

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NASA Technical Paper

NASA Technical Paper PDF Author:
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ISBN:
Category : Astronautics
Languages : en
Pages : 524

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
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Category : Mechanics, Applied
Languages : en
Pages : 742

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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Category : Government publications
Languages : en
Pages : 1320

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
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Category : United States
Languages : en
Pages : 1348

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 2300

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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Category : Aeronautics
Languages : en
Pages : 2088

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A Selected Listing of NASA Scientific and Technical Reports for 1966

A Selected Listing of NASA Scientific and Technical Reports for 1966 PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2084

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