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

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 ...

An improved transverse shear deformation theory for laminated anisotropic plates /

Murthy, M. V. V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

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...

Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading /

Hong, C. S.
Crews, John H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Includes statistical tables.Includes bibliographical references."May 1979"--Cover."Langley Research ...

Elastic stress distribution in a finite-width orthotropic plate containing a crack /

Mendelson, Alexander.
Spero, Samuel W.
Lewis Research Center.

Prepared at Lewis Research Center."March 1964"--Cover.Includes bibliographical references (p. 16).Mo...

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...

Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet /

Bigelow, C. A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986."Includes bibliographical references (p. 11).Mode ...

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

Raju, I. S.
Hong, C. S.
Crews, J. H., Jr.

May 1981

Stresses were calculated for finite size orthotropic laminates loaded by a frictionless steel pin in...

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 ...

Stress concentrations in filamentary structures. /

Hedgepeth, John M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

A critical examination of stresses in an elastic single lap joint /

Cooper, Paul A.
Sawyer, James Wayne, 1941-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"September 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle /

Sova, J. A.
Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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 ...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

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...

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 ...

An improved transverse shear deformation theory for laminated anisotropic plates /

Murthy, M. V. V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

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...

Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading /

Hong, C. S.
Crews, John H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Includes statistical tables.Includes bibliographical references."May 1979"--Cover."Langley Research ...

Elastic stress distribution in a finite-width orthotropic plate containing a crack /

Mendelson, Alexander.
Spero, Samuel W.
Lewis Research Center.

Prepared at Lewis Research Center."March 1964"--Cover.Includes bibliographical references (p. 16).Mo...

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...

Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet /

Bigelow, C. A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986."Includes bibliographical references (p. 11).Mode ...

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

Raju, I. S.
Hong, C. S.
Crews, J. H., Jr.

May 1981

Stresses were calculated for finite size orthotropic laminates loaded by a frictionless steel pin in...

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 ...

Stress concentrations in filamentary structures. /

Hedgepeth, John M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

A critical examination of stresses in an elastic single lap joint /

Cooper, Paul A.
Sawyer, James Wayne, 1941-
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

"September 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle /

Sova, J. A.
Crews, John H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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 ...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

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...

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 ...

An improved transverse shear deformation theory for laminated anisotropic plates /

Murthy, M. V. V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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