Analysis of graphite/polyimide rail shear specimens subjected to mechnaical and thermal loading /

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...

Tensile properties of aircraft-structural metals at various rates of loading after rapid heating /

Kattus, J. R., author.
United States. Air Force. Air Research and Development Command. issuing body.
Wright Air Development Center sponsor.
Southern Research Institute (Birmingham, Ala.), sponsor.

"May 1959."ASTIA document no. 213834.Includes bibliographical references (pages 44-46).Prepared by t...

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 ...

Buckling and failure characteristics of graphite-polyimide shear panels /

Shuart, Mark J.
Hagaman, Jane A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"May 1983"--Cover.Subject category 24.Distributed to depository libraries in microfiche.Includes bib...

Experimental data on single-bolt joints in quasi-isotropic graphite/polyimide laminates /

Wichorek, Gregory R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 24."Langley Research Center.""May 1982"--Cover.Includes bibliographical references....

Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression /

Sydow, P. Daniel.
Shuart, Mark J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Tests of graphite/polymide sandwich panels in uniaxial edgewise compression /

Camarda, Charles J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

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...

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 ...

Elevated-temperature application of the IITRI compression test fixture for graphite/polyimide filmentary composites /

Raju, B. Basava.
Cooper, Paul A.
Camarda, Charles J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 24."September 1979"--Cover."Langley Research Center."Includes bibliographical refer...

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: ...

Shear-lag analysis of notched laminates with interlaminar debonding /

Goree, J. G.
Kaw, Autar K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Clemson University.
Langley Research Center.

January 1984

"Clemson University."Subject category 24."May 1984"--Cover.Distributed to depository libraries in mi...

Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading /

Wichorek, Gregory R.
Crews, John H.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 8)...

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 ...

The interlaminar fracture toughness of woven graphite/epoxy composites /

Funk, Joan G.
Deaton, Jerry W.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 6.Mode of access: Internet

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...

Tensile properties of aircraft-structural metals at various rates of loading after rapid heating /

Kattus, J. R., author.
United States. Air Force. Air Research and Development Command. issuing body.
Wright Air Development Center sponsor.
Southern Research Institute (Birmingham, Ala.), sponsor.

"May 1959."ASTIA document no. 213834.Includes bibliographical references (pages 44-46).Prepared by t...

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 ...

Buckling and failure characteristics of graphite-polyimide shear panels /

Shuart, Mark J.
Hagaman, Jane A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"May 1983"--Cover.Subject category 24.Distributed to depository libraries in microfiche.Includes bib...

Experimental data on single-bolt joints in quasi-isotropic graphite/polyimide laminates /

Wichorek, Gregory R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 24."Langley Research Center.""May 1982"--Cover.Includes bibliographical references....

Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression /

Sydow, P. Daniel.
Shuart, Mark J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Tests of graphite/polymide sandwich panels in uniaxial edgewise compression /

Camarda, Charles J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

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...

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 ...

Elevated-temperature application of the IITRI compression test fixture for graphite/polyimide filmentary composites /

Raju, B. Basava.
Cooper, Paul A.
Camarda, Charles J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject Category 24."September 1979"--Cover."Langley Research Center."Includes bibliographical refer...

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: ...

Shear-lag analysis of notched laminates with interlaminar debonding /

Goree, J. G.
Kaw, Autar K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Clemson University.
Langley Research Center.

January 1984

"Clemson University."Subject category 24."May 1984"--Cover.Distributed to depository libraries in mi...

Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading /

Wichorek, Gregory R.
Crews, John H.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 8)...

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 ...

The interlaminar fracture toughness of woven graphite/epoxy composites /

Funk, Joan G.
Deaton, Jerry W.
Langley Research Center.

January 1989

Research performed at Langley Research Center.Bibliography: p. 6.Mode of access: Internet

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...

Tensile properties of aircraft-structural metals at various rates of loading after rapid heating /

Kattus, J. R., author.
United States. Air Force. Air Research and Development Command. issuing body.
Wright Air Development Center sponsor.
Southern Research Institute (Birmingham, Ala.), sponsor.

"May 1959."ASTIA document no. 213834.Includes bibliographical references (pages 44-46).Prepared by t...

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 of graphite/polyimide rail shear specimens subjected to mechnaical and thermal loading /

Abstract

Extracted data

Analysis of graphite/polyimide rail shear specimens subjected to mechnaical and thermal loading /

Abstract

Extracted data

Topics

Related items

Topics

Related items