The fatigue behavior of materials for the supersonic transport /

Tension, compression, and fatigue properties of several SAE 52100 and tool steels used for ball bearings /

Sachs, G.
Weiss, V.
Sell, R.
Langley Research Center.

January 1960

"NASA TN D-239.""Langley Research Center, Langley Field, Va.""February 1960."Cover title.Includes bi...

Some considerations in the fatigue design of launch and spacecraft structures /

Christensen, R. H.
Bellinfante, R. J.
Douglas Aircraft Company.

January 1965

"Prepared under Contract No. NAS 7-298 by Douglas Aircraft Company, Inc."Includes bibliographical re...

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

An approach to metal fatigue /

Stulen, F. B.
Schulte, W. C.
Redfern, J. H.
Curtiss-Wright Corporation.
United States. National Aeronautics and Space Administration.

January 1965

"June 1965"--- title page.Includes bibliographical references (p. 32-34).Prepared by Curtiss-Wright ...

Effects of longtime environmental exposure on mechanical properties of sheet materials for a supersonic transport /

Pride, Richard A. (Richard Allen), 1922-
Langley Research Center.

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 12)....

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...

Thermal fatigue of ductile materials.

Clauss, Francis J.
Lewis Research Center.

January 1959

"NASA TN D-69.""Lewis Research Center, Cleveland, Ohio.""October 1959."Title from cover.Includes bib...

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 ...

Consolidation of fatigue and fatigue-crack-propagation data for design use /

Rice, Richard C.
Langley Research Center.
Battelle Memorial Institute. Columbus Laboratories.

"Prepared by Battelle Columbus Laboratories ... for Langley Research Center.""October 1975."Cover ti...

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...

A study of the acoustic fatigue characteristics of some flat and curved aluminum panels exposed to random and discrete noise /

Hess, R. W. (Robert W.)
Mayes, William H.
Herr, Robert W.
Langley Research Center.

January 1959

"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

The mechanical properties at 800,̊ 1000,̊ and 1200 ̊F of two superalloys under consideration for use in the supersonic transport /

Cullen, T. M.
Freeman, J. W.
University of Michigan.
United States. National Aeronautics and Space Administration.

"September 1964"--- cover.Includes bibliographical references (p. 17).Prepared by University of Mich...

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

The fatigue behavior of materials for the supersonic transport

Marshall, C. W.
Hyler, W. S.
Holden, F. C.
Healy, M. S.

April 1965

Crack propagation behavior, residual static strength, and base fatigue strength of supersonic transp...

Tension, compression, and fatigue properties of several SAE 52100 and tool steels used for ball bearings /

Sachs, G.
Weiss, V.
Sell, R.
Langley Research Center.

January 1960

"NASA TN D-239.""Langley Research Center, Langley Field, Va.""February 1960."Cover title.Includes bi...

Some considerations in the fatigue design of launch and spacecraft structures /

Christensen, R. H.
Bellinfante, R. J.
Douglas Aircraft Company.

January 1965

"Prepared under Contract No. NAS 7-298 by Douglas Aircraft Company, Inc."Includes bibliographical re...

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

An approach to metal fatigue /

Stulen, F. B.
Schulte, W. C.
Redfern, J. H.
Curtiss-Wright Corporation.
United States. National Aeronautics and Space Administration.

January 1965

"June 1965"--- title page.Includes bibliographical references (p. 32-34).Prepared by Curtiss-Wright ...

Effects of longtime environmental exposure on mechanical properties of sheet materials for a supersonic transport /

Pride, Richard A. (Richard Allen), 1922-
Langley Research Center.

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 12)....

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...

Thermal fatigue of ductile materials.

Clauss, Francis J.
Lewis Research Center.

January 1959

"NASA TN D-69.""Lewis Research Center, Cleveland, Ohio.""October 1959."Title from cover.Includes bib...

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 ...

Consolidation of fatigue and fatigue-crack-propagation data for design use /

Rice, Richard C.
Langley Research Center.
Battelle Memorial Institute. Columbus Laboratories.

"Prepared by Battelle Columbus Laboratories ... for Langley Research Center.""October 1975."Cover ti...

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...

A study of the acoustic fatigue characteristics of some flat and curved aluminum panels exposed to random and discrete noise /

Hess, R. W. (Robert W.)
Mayes, William H.
Herr, Robert W.
Langley Research Center.

January 1959

"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

The mechanical properties at 800,̊ 1000,̊ and 1200 ̊F of two superalloys under consideration for use in the supersonic transport /

Cullen, T. M.
Freeman, J. W.
University of Michigan.
United States. National Aeronautics and Space Administration.

"September 1964"--- cover.Includes bibliographical references (p. 17).Prepared by University of Mich...

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

The fatigue behavior of materials for the supersonic transport

Marshall, C. W.
Hyler, W. S.
Holden, F. C.
Healy, M. S.

April 1965

Crack propagation behavior, residual static strength, and base fatigue strength of supersonic transp...

Tension, compression, and fatigue properties of several SAE 52100 and tool steels used for ball bearings /

Sachs, G.
Weiss, V.
Sell, R.
Langley Research Center.

January 1960

"NASA TN D-239.""Langley Research Center, Langley Field, Va.""February 1960."Cover title.Includes bi...

Some considerations in the fatigue design of launch and spacecraft structures /

Christensen, R. H.
Bellinfante, R. J.
Douglas Aircraft Company.

January 1965

"Prepared under Contract No. NAS 7-298 by Douglas Aircraft Company, Inc."Includes bibliographical re...

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

The fatigue behavior of materials for the supersonic transport /

Abstract

Extracted data

The fatigue behavior of materials for the supersonic transport /

Abstract

Extracted data

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