Residual static strength of aluminum-alloy box beams containing fatigue cracks in the tension covers /

General theory of large deflections of thin shells /

Dill, E. H.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Stresses and loads; StructuresIncludes bibliographical references.Mode of a...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Determination of the creep deflection and lifetime of aluminum-alloy multiweb box beams subjected to varied loads at constant temperature /

Berkovits, Avraham.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inter...

Fatigue investigation of full-scale wing panels of 7075 aluminum alloy /

Castle, Claude B.
Ward, John F.
United States. National Aeronautics and Space Administration.

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

Preliminary results of stability calculations for the bending of box beams with longitudinally stiffened covers connected by posts /

Anderson, Roger A.
Johnson, Aldie E.
Wilder Thomas W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"December 1, 1952."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Tensile properties and sheet-bending fatigue properties of some refractory metals at room temperature

Foster, Lee R.
Stein, Bland A.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading /

Simonds, R. A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Langley Research Center.

January 1984

Subject category 24."July 1984"--Cover.Distributed to depository libraries in microfiche."Virginia P...

Crack propagation, delayed failure, and residual static strength of titanium, aluminum, and stainless steel alloys in aqueous environments /

Figge, I. E.
Hudson, C. Michael.
Langley Research Center.

January 1967

"February 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Fatigue damage under varying stress amplitudes /

Liu, H. W. (Hao Wen), 1926-
Corten, H. T. (Herbert Theodore)
University of Illinois (Urbana-Champaign campus)

Prepared at the University of Illinois."November 1960."Cover title.Includes bibliographical referenc...

Analytical study of creep deflection of structural beams /by Leonard Mordfin.

Mordfin, Leonard.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Stresses and loads; Structures.Includes bibliographical references.Mode ...

Investigation of tapered circular reinforcements around central holes in flat sheets under biaxial loads in the elastic range /

Kaufman, Albert
Morgan, William C.
Bizon, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Stresses and loads; Structures.Includes bibliographical references.Mode ...

Strength and stiffness of reinforced yellow-poplar glued-laminated beams /

Hernandez, Roland.
Forest Products Laboratory (U.S.)

"July 1997"--P. [2] of cover.Cover title.Includes bibliographical references (p. 12-13).Mode of acce...

Unified notch-strength analysis for wrought aluminum alloys. Paul Kuhn and I.E. Figge.

Kuhn, Paul.
Figge, I. E.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Materials, engineering; Stresses and loads; Structures.Includes bibliographic...

General theory of large deflections of thin shells /

Dill, E. H.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Stresses and loads; StructuresIncludes bibliographical references.Mode of a...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Determination of the creep deflection and lifetime of aluminum-alloy multiweb box beams subjected to varied loads at constant temperature /

Berkovits, Avraham.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inter...

Fatigue investigation of full-scale wing panels of 7075 aluminum alloy /

Castle, Claude B.
Ward, John F.
United States. National Aeronautics and Space Administration.

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

Preliminary results of stability calculations for the bending of box beams with longitudinally stiffened covers connected by posts /

Anderson, Roger A.
Johnson, Aldie E.
Wilder Thomas W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"December 1, 1952."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Tensile properties and sheet-bending fatigue properties of some refractory metals at room temperature

Foster, Lee R.
Stein, Bland A.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Residual strength of five boron/aluminum laminates with crack-like notches after fatigue loading /

Simonds, R. A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Langley Research Center.

January 1984

Subject category 24."July 1984"--Cover.Distributed to depository libraries in microfiche."Virginia P...

Crack propagation, delayed failure, and residual static strength of titanium, aluminum, and stainless steel alloys in aqueous environments /

Figge, I. E.
Hudson, C. Michael.
Langley Research Center.

January 1967

"February 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Fatigue damage under varying stress amplitudes /

Liu, H. W. (Hao Wen), 1926-
Corten, H. T. (Herbert Theodore)
University of Illinois (Urbana-Champaign campus)

Prepared at the University of Illinois."November 1960."Cover title.Includes bibliographical referenc...

Analytical study of creep deflection of structural beams /by Leonard Mordfin.

Mordfin, Leonard.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Stresses and loads; Structures.Includes bibliographical references.Mode ...

Investigation of tapered circular reinforcements around central holes in flat sheets under biaxial loads in the elastic range /

Kaufman, Albert
Morgan, William C.
Bizon, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Stresses and loads; Structures.Includes bibliographical references.Mode ...

Strength and stiffness of reinforced yellow-poplar glued-laminated beams /

Hernandez, Roland.
Forest Products Laboratory (U.S.)

"July 1997"--P. [2] of cover.Cover title.Includes bibliographical references (p. 12-13).Mode of acce...

Unified notch-strength analysis for wrought aluminum alloys. Paul Kuhn and I.E. Figge.

Kuhn, Paul.
Figge, I. E.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Materials, engineering; Stresses and loads; Structures.Includes bibliographic...

General theory of large deflections of thin shells /

Dill, E. H.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Stresses and loads; StructuresIncludes bibliographical references.Mode of a...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Stress-corrosion cracking of aluminum alloys /

Jackson, J. D. author.
Boyd, Walter K., author.
Defense Metals Information Center (U.S.) issuing body.

Research supported by the Technology Division, Wright-Patterson Air Force Base, Ohio.Cover title."Fe...

Residual static strength of aluminum-alloy box beams containing fatigue cracks in the tension covers /

Abstract

Extracted data

Residual static strength of aluminum-alloy box beams containing fatigue cracks in the tension covers /

Abstract

Extracted data

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