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

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...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

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...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

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 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...

Flutter of elastically supported orthotropic panels including the effects of flow angle /

Sawyer, James Wayne, 1941-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode ...

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...

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

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

Housner, J. M.
Stein, M.

October 1975

A computer program is presented which was developed for the combined compression and shear of stiffe...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Classical buckling of cylinders of sandwich construction in axial compression : orthotropic cores /

Zahn, John J., 1932-

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

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 ...

A new look at numerical analyses of free-edge stresses in composite laminates /

Raju, I. S.
Goree, J. G.
Whitcomb, J. D.
Langley Research Center.
Joint Institute for Advancement of Flight Sciences.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center.""The George Washington University, Joint Institute for Advanceme...

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

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...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

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...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

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 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...

Flutter of elastically supported orthotropic panels including the effects of flow angle /

Sawyer, James Wayne, 1941-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode ...

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...

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

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

Housner, J. M.
Stein, M.

October 1975

A computer program is presented which was developed for the combined compression and shear of stiffe...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Classical buckling of cylinders of sandwich construction in axial compression : orthotropic cores /

Zahn, John J., 1932-

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

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 ...

A new look at numerical analyses of free-edge stresses in composite laminates /

Raju, I. S.
Goree, J. G.
Whitcomb, J. D.
Langley Research Center.
Joint Institute for Advancement of Flight Sciences.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center.""The George Washington University, Joint Institute for Advanceme...

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

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...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items