Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression

Design and Analysis of Stiffened Composite Panels Including Postbuckling and Collapse

Degenhardt, Richard
Kling, Alexander
Rohwer, Klaus
Orifici, A.
Thomson, R.S.

January 2007

he European aircraft industry demands reduced development and operating costs, by 20% and 50% in the...

National Aeronautics and Space Administration

William L. Ko
Raymond H. Jackson
William L. Ko
Raymond H. Jackson
Shear Buckling Analysis

January 1994

of a Hat-Stiffened Panel A buckling analysis was performed on a hat-stiffened panel subjected to she...

Post-buckling behaviour of uniform cellular structures

Costa, P.M.M.P. da Providencia

January 1994

SIGLEAvailable from British Library Document Supply Centre-DSC:DX189824 / BLDSC - British Library Do...

A finite element study of the postbuckling behaviour of a typical aircraft fuselage panel

Lynch, C.J.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN042976 / BLDSC - British Library D...

An investigation into the compressive strength and stability characteristics of welded aircraft fuselage panels

Gibson, A.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN036250 / BLDSC - British Library D...

Buckling of flat plates and cylindrical panels under complex load cases

Featherston, C.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199185 / BLDSC - British Library Doc...

Aircraft wing panel buckling analysis: efficiency by approximations

York, C.B.
Williams, F.W.

September 1998

A comparison of ‘exact’ and approximate methods for the determination of critical buckling loads of ...

Post-Buckled Composite Panels for Helicopter Fuselages: Design, Analysis, Fabrication and Testing

February 2008

For the lightly-loaded structures (200 lbs/in. in compression and 400 lbs/in. in shear), the traditi...

Buckling loads of flat sandwich panels in compression : The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate)

January 1960

This report is one of a series issued in cooperation withe the Army-Navy-Civil Committee on aircraft...

The stability and post-buckling behaviour of stiffened plates in compression

Jhita, P
Cranfield Inst. of Tech. (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX92929 / BLDSC - British Library Do...

Buckling loads of stiffened panels subjected to combined longitudinal compression and shear : results obtained with PASCO, EAL, and STAGS computer programs /

Stroud, W. Jefferson
Anderson, Melvin S.
Greene, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39.Distributed to depository libraries in microfiche."January 1984"--Cover.Includes...

The large deflection elasto-plastic analysis of double-span stiffened panels under uni-axial compression

Lin, Y.T.
Frieze, P.A
Glasgow Univ. (United Kingdom). Dept. of Naval Architecture and Ocean Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:9110.2555(NAOE--85-55) / BLDSC - Bri...

Experiments on Buckling and Postbuckling of Thin-Walled CFRP Structures using Advanced Measurement Systems

Degenhardt, Richard
Kling, Alexander
Hillger, Wolfgang
Goetting, Hans Christian
Zimmermann, Rolf
Rohwer, Klaus
Gleiter, Andreas

June 2007

The aircraft and space industry strives for significantly reduced development and operating costs. R...

Buckling tests on one-sided single-stiffener panels

Frey, P.M
Cambridge Univ. (United Kingdom). Dept. of Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/D-STRUCT/TR--113) / BLD...

Buckling Analysis of Fuselage Frame Using CAD/CAM Software

, Dr. M. Satheesh, Mr. Arun M P

November 2017

The objective of this project is to study the strength of an aircraft fuselage when subjected to buc...

Design and Analysis of Stiffened Composite Panels Including Postbuckling and Collapse

Degenhardt, Richard
Kling, Alexander
Rohwer, Klaus
Orifici, A.
Thomson, R.S.

January 2007

he European aircraft industry demands reduced development and operating costs, by 20% and 50% in the...

National Aeronautics and Space Administration

William L. Ko
Raymond H. Jackson
William L. Ko
Raymond H. Jackson
Shear Buckling Analysis

January 1994

of a Hat-Stiffened Panel A buckling analysis was performed on a hat-stiffened panel subjected to she...

Post-buckling behaviour of uniform cellular structures

Costa, P.M.M.P. da Providencia

January 1994

SIGLEAvailable from British Library Document Supply Centre-DSC:DX189824 / BLDSC - British Library Do...

A finite element study of the postbuckling behaviour of a typical aircraft fuselage panel

Lynch, C.J.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN042976 / BLDSC - British Library D...

An investigation into the compressive strength and stability characteristics of welded aircraft fuselage panels

Gibson, A.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN036250 / BLDSC - British Library D...

Buckling of flat plates and cylindrical panels under complex load cases

Featherston, C.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199185 / BLDSC - British Library Doc...

Aircraft wing panel buckling analysis: efficiency by approximations

York, C.B.
Williams, F.W.

September 1998

A comparison of ‘exact’ and approximate methods for the determination of critical buckling loads of ...

Post-Buckled Composite Panels for Helicopter Fuselages: Design, Analysis, Fabrication and Testing

February 2008

For the lightly-loaded structures (200 lbs/in. in compression and 400 lbs/in. in shear), the traditi...

Buckling loads of flat sandwich panels in compression : The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate)

January 1960

This report is one of a series issued in cooperation withe the Army-Navy-Civil Committee on aircraft...

The stability and post-buckling behaviour of stiffened plates in compression

Jhita, P
Cranfield Inst. of Tech. (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX92929 / BLDSC - British Library Do...

Buckling loads of stiffened panels subjected to combined longitudinal compression and shear : results obtained with PASCO, EAL, and STAGS computer programs /

Stroud, W. Jefferson
Anderson, Melvin S.
Greene, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39.Distributed to depository libraries in microfiche."January 1984"--Cover.Includes...

The large deflection elasto-plastic analysis of double-span stiffened panels under uni-axial compression

Lin, Y.T.
Frieze, P.A
Glasgow Univ. (United Kingdom). Dept. of Naval Architecture and Ocean Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:9110.2555(NAOE--85-55) / BLDSC - Bri...

Experiments on Buckling and Postbuckling of Thin-Walled CFRP Structures using Advanced Measurement Systems

Degenhardt, Richard
Kling, Alexander
Hillger, Wolfgang
Goetting, Hans Christian
Zimmermann, Rolf
Rohwer, Klaus
Gleiter, Andreas

June 2007

The aircraft and space industry strives for significantly reduced development and operating costs. R...

Buckling tests on one-sided single-stiffener panels

Frey, P.M
Cambridge Univ. (United Kingdom). Dept. of Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/D-STRUCT/TR--113) / BLD...

Buckling Analysis of Fuselage Frame Using CAD/CAM Software

, Dr. M. Satheesh, Mr. Arun M P

November 2017

The objective of this project is to study the strength of an aircraft fuselage when subjected to buc...

Design and Analysis of Stiffened Composite Panels Including Postbuckling and Collapse

Degenhardt, Richard
Kling, Alexander
Rohwer, Klaus
Orifici, A.
Thomson, R.S.

January 2007

he European aircraft industry demands reduced development and operating costs, by 20% and 50% in the...

National Aeronautics and Space Administration

William L. Ko
Raymond H. Jackson
William L. Ko
Raymond H. Jackson
Shear Buckling Analysis

January 1994

of a Hat-Stiffened Panel A buckling analysis was performed on a hat-stiffened panel subjected to she...

Post-buckling behaviour of uniform cellular structures

Costa, P.M.M.P. da Providencia

January 1994

SIGLEAvailable from British Library Document Supply Centre-DSC:DX189824 / BLDSC - British Library Do...

Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression

Abstract

Extracted data

Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression

Abstract

Extracted data

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