Effect of specimen thickness on fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys /

Compressive and tensile creep of 7075-T6 and 2024-T3 aluminum-alloy sheet /

Heimerl, George J.
Farquhar, John, 1932-
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system /

Sova, J. A.
Exton, R. J., joint author.
Crews, John H., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16-17).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...

Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys /

Everett, Richard A.
Langley Research Center.

January 1975

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

Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens /

Hudson, C. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Stress ratio effects on fatigue crack growth in sheet aluminum alloys.Prepared at Langley Research C...

Fatigue-crack-propagation and fracture-toughness characteristics of 7079 aluminum-alloy sheets and plates in three aged conditions,

Smith, S. H. (Samuel Harrison), 1937-
Sump, W. D., joint author.
Porter, T. R., joint author.
Langley Research Center.
Boeing Company.

"Prepared under contract no. NAS 1-6474 by the Boeing Company, Renton, Wash. for Langley Research Ce...

Effect of specimen thickness of fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys

Newman, J. C., Jr.
Hudson, C. M.

April 1973

A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...

Load interaction effects on fatigue crack growth in Ti-6Al-4V alloy /

Wei, Robert Peh-ying, 1931-
FitzGerald, J. H.
Shih, T. T.
Langley Research Center.
Lehigh University.

January 1973

"Prepared by Lehigh University ... for Langley Research Center."Cover title.Bibliography: p. 10.Mode...

Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K)

Royster, Dick M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 12...

Crack-closure and crack-growth measurements in surface-flawed titanium alloy Ti-6Al-4V /

Wolf, Elber.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels /

Hudson, Charles Michael, 1935-
Lewis, Peter E.
Newman, J. C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

A study of crack closure in fatigue /

Shih, T. T.
Wei, Robert Peh-ying, 1931-
Langley Research Center.
Lehigh University.

January 1973

"Prepared by Lehigh University ... for Langley Research Center."Cover title.Bibliography: p. 74-76.M...

Fracture toughness of boron/aluminum laminates with various proportions of 0° and ±45 ̊plies /

Poe, C. C.
Sova, J. A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

Failure analysis of aluminum alloy components /

Johari, Om.
Staschke, Joseph.
Corvin, Irene.
Langley Research Center.
IIT Research Institute.

January 1973

"Prepared by IIT Research Institute ... for Langley Research Center."Cover title.Bibliography: p. 69...

Crack-growth behavior in thick welded plates of Inconel 718 at room and cryogenic temperatures /

Forman, Royce G.
Lyndon B. Johnson Space Center.

January 1974

Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 17).Mode of acc...

Compressive and tensile creep of 7075-T6 and 2024-T3 aluminum-alloy sheet /

Heimerl, George J.
Farquhar, John, 1932-
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system /

Sova, J. A.
Exton, R. J., joint author.
Crews, John H., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16-17).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...

Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys /

Everett, Richard A.
Langley Research Center.

January 1975

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

Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens /

Hudson, C. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Stress ratio effects on fatigue crack growth in sheet aluminum alloys.Prepared at Langley Research C...

Fatigue-crack-propagation and fracture-toughness characteristics of 7079 aluminum-alloy sheets and plates in three aged conditions,

Smith, S. H. (Samuel Harrison), 1937-
Sump, W. D., joint author.
Porter, T. R., joint author.
Langley Research Center.
Boeing Company.

"Prepared under contract no. NAS 1-6474 by the Boeing Company, Renton, Wash. for Langley Research Ce...

Effect of specimen thickness of fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys

Newman, J. C., Jr.
Hudson, C. M.

April 1973

A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...

Load interaction effects on fatigue crack growth in Ti-6Al-4V alloy /

Wei, Robert Peh-ying, 1931-
FitzGerald, J. H.
Shih, T. T.
Langley Research Center.
Lehigh University.

January 1973

"Prepared by Lehigh University ... for Langley Research Center."Cover title.Bibliography: p. 10.Mode...

Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K)

Royster, Dick M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 12...

Crack-closure and crack-growth measurements in surface-flawed titanium alloy Ti-6Al-4V /

Wolf, Elber.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 7).Mode of a...

An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels /

Hudson, Charles Michael, 1935-
Lewis, Peter E.
Newman, J. C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

A study of crack closure in fatigue /

Shih, T. T.
Wei, Robert Peh-ying, 1931-
Langley Research Center.
Lehigh University.

January 1973

"Prepared by Lehigh University ... for Langley Research Center."Cover title.Bibliography: p. 74-76.M...

Fracture toughness of boron/aluminum laminates with various proportions of 0° and ±45 ̊plies /

Poe, C. C.
Sova, J. A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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

Failure analysis of aluminum alloy components /

Johari, Om.
Staschke, Joseph.
Corvin, Irene.
Langley Research Center.
IIT Research Institute.

January 1973

"Prepared by IIT Research Institute ... for Langley Research Center."Cover title.Bibliography: p. 69...

Crack-growth behavior in thick welded plates of Inconel 718 at room and cryogenic temperatures /

Forman, Royce G.
Lyndon B. Johnson Space Center.

January 1974

Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 17).Mode of acc...

Compressive and tensile creep of 7075-T6 and 2024-T3 aluminum-alloy sheet /

Heimerl, George J.
Farquhar, John, 1932-
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system /

Sova, J. A.
Exton, R. J., joint author.
Crews, John H., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16-17).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...

Effect of specimen thickness on fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys /

Abstract

Extracted data

Effect of specimen thickness on fatigue-crack-growth behavior and fracture toughness of 7075-T6 and 7178-T6 aluminum alloys /

Abstract

Extracted data

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