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

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

Tensile behavior of boron/epoxy-reinforced 7075-T6 aluminum alloy at elevated temperatures /

Chwirut, Daniel J.
Sushinsky, George F.
United States. National Bureau of Standards.

January 1974

Sponsored by the National Aeronautics and Space Administration, Langley Research Center.Mode of acce...

A novel method of testing the shear strength of thick honeycomb composites /

Hodge, A. J.
Nettles, A. T. (Alan T.)
George C. Marshall Space Flight Center.

January 1991

Prepared at the George C. Marshall Space Flight Center.Bibliography: p. 10.Mode of access: Internet

Compressive buckling analysis of hat-stiffened panel /

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

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.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...

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 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...

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 ...

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

Ko, William L.
Jackson, Raymond H.

September 1991

Combined compressive and shear buckling analysis was conducted on flat rectangular sandwich panels w...

Edgewise compressive buckling of flat sandwich panels : loaded ends simply supported and sides supported by beams /

Zahn, John J., 1932-

"This report is one of a series issued in cooperation with the MIL-HDBK-23 Working Group on Composit...

Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

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...

Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads /

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

January 1974

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

Fiber-reinforced metal-matrix composites--1969-1970 /

Hanby, K. R. (Kenneth Roger), author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio."July 1, 1971."...

Buckling coefficients for sandwich cylinders of finite length under uniform external lateral pressure /

Kuenzi, Edward W.
Stevens, G. H. (Gordon H.)
Bohannan, Billy.
University of Wisconsin.
Forest Products Laboratory (U.S.)

"September 1965.""This report is one of a series issued in cooperation with the MIL-HDBK-23 Working ...

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

Tensile behavior of boron/epoxy-reinforced 7075-T6 aluminum alloy at elevated temperatures /

Chwirut, Daniel J.
Sushinsky, George F.
United States. National Bureau of Standards.

January 1974

Sponsored by the National Aeronautics and Space Administration, Langley Research Center.Mode of acce...

A novel method of testing the shear strength of thick honeycomb composites /

Hodge, A. J.
Nettles, A. T. (Alan T.)
George C. Marshall Space Flight Center.

January 1991

Prepared at the George C. Marshall Space Flight Center.Bibliography: p. 10.Mode of access: Internet

Compressive buckling analysis of hat-stiffened panel /

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

January 1991

Prepared at Dryden Flight Research Facility.Bibliography: p. 9.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...

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 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...

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 ...

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

Ko, William L.
Jackson, Raymond H.

September 1991

Combined compressive and shear buckling analysis was conducted on flat rectangular sandwich panels w...

Edgewise compressive buckling of flat sandwich panels : loaded ends simply supported and sides supported by beams /

Zahn, John J., 1932-

"This report is one of a series issued in cooperation with the MIL-HDBK-23 Working Group on Composit...

Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

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...

Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads /

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

January 1974

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

Fiber-reinforced metal-matrix composites--1969-1970 /

Hanby, K. R. (Kenneth Roger), author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio."July 1, 1971."...

Buckling coefficients for sandwich cylinders of finite length under uniform external lateral pressure /

Kuenzi, Edward W.
Stevens, G. H. (Gordon H.)
Bohannan, Billy.
University of Wisconsin.
Forest Products Laboratory (U.S.)

"September 1965.""This report is one of a series issued in cooperation with the MIL-HDBK-23 Working ...

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

Tensile behavior of boron/epoxy-reinforced 7075-T6 aluminum alloy at elevated temperatures /

Chwirut, Daniel J.
Sushinsky, George F.
United States. National Bureau of Standards.

January 1974

Sponsored by the National Aeronautics and Space Administration, Langley Research Center.Mode of acce...

A novel method of testing the shear strength of thick honeycomb composites /

Hodge, A. J.
Nettles, A. T. (Alan T.)
George C. Marshall Space Flight Center.

January 1991

Prepared at the George C. Marshall Space Flight Center.Bibliography: p. 10.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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