Compressive buckling analysis of hat-stiffened panel /

Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder /

Davis, Randall C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."Langley Research Center.""July 1982"--Cover.Includes bibliographical references...

Computer analysis of ring-stiffened shells of revolution /

Cohen, Gerald A.
Langley Research Center.
Structures Research Associates.

January 1973

"Prepared by Structures Research Associates ... for Langley Research Center."Cover title.Bibliograph...

Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 14.Mode of access: Internet

Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads /

Viswanathan, A. V.
Tamekuni, M.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1973

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Bib...

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Minimum-weight designs for hat-stiffened composite panels under uniaxial compression /

Agarwal, Banarsi.
Davis, Randall C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode ...

Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 12.Mode of access: Internet

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

Analysis and testing of axial compression in imperfect slender truss struts /

Lake, Mark S.
Georgiadis, Nicholas, 1925-2001.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts /

Nemeth, Michael P.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /

Ko, William L.
Muramoto, Kyle M.
Olona, Timothy.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Optimization of composite sandwich cover panels subjected to compressive loadings /

Cruz, Juan R.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

Buckling tests of two integrally stiffened cylinders subjected to bending /

Anderson, James Kent.
Peterson, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1975

Prepared at Langley Research Center.N 71-28116.Includes bibliographical references (p. 9).Mode of ac...

Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder /

Davis, Randall C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."Langley Research Center.""July 1982"--Cover.Includes bibliographical references...

Computer analysis of ring-stiffened shells of revolution /

Cohen, Gerald A.
Langley Research Center.
Structures Research Associates.

January 1973

"Prepared by Structures Research Associates ... for Langley Research Center."Cover title.Bibliograph...

Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 14.Mode of access: Internet

Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads /

Viswanathan, A. V.
Tamekuni, M.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1973

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center."Cover title.Bib...

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Minimum-weight designs for hat-stiffened composite panels under uniaxial compression /

Agarwal, Banarsi.
Davis, Randall C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode ...

Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 12.Mode of access: Internet

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

Analysis and testing of axial compression in imperfect slender truss struts /

Lake, Mark S.
Georgiadis, Nicholas, 1925-2001.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts /

Nemeth, Michael P.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Development of an integrated aeroservoelastic analysis program and correlation with test data /

Gupta, Kajal K.
Voelker, L. S.
Brenner, M. J.
Dryden Flight Research Facility.

January 1991

Prepared at the Dryden Flight Research Facility.Bibliography: p. 39.Mode of access: Internet

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures /

Ko, William L.
Muramoto, Kyle M.
Olona, Timothy.
Dryden Flight Research Facility.

January 1990

Prepared at Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Optimization of composite sandwich cover panels subjected to compressive loadings /

Cruz, Juan R.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 9).Mode of access: Inter...

Buckling tests of two integrally stiffened cylinders subjected to bending /

Anderson, James Kent.
Peterson, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1975

Prepared at Langley Research Center.N 71-28116.Includes bibliographical references (p. 9).Mode of ac...

Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder /

Davis, Randall C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."Langley Research Center.""July 1982"--Cover.Includes bibliographical references...

Computer analysis of ring-stiffened shells of revolution /

Cohen, Gerald A.
Langley Research Center.
Structures Research Associates.

January 1973

"Prepared by Structures Research Associates ... for Langley Research Center."Cover title.Bibliograph...

Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments /

Ko, William L.
Jackson, Raymond H.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Bibliography: p. 14.Mode of access: Internet

Compressive buckling analysis of hat-stiffened panel /

Abstract

Extracted data

Compressive buckling analysis of hat-stiffened panel /

Abstract

Extracted data

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