Author: Michael F. Card
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Preliminary Results of Compression Tests on Cylinders with Eccentric Longitudinal Stiffeners
NASA Technical Note
Test Methods for Compression Members
Author:
Publisher: ASTM International
ISBN:
Category : Columns
Languages : en
Pages : 221
Book Description
Publisher: ASTM International
ISBN:
Category : Columns
Languages : en
Pages : 221
Book Description
Proceedings
Author: International Council of the Aeronautical Sciences
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
Book Description
The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression
Author: John N. Dickson
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 44
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.
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 44
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.
Aerospace Proceedings, 1966
Author: Joan Bradbrooke
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 576
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 576
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
Book Description