Tensile and compressive creep of 6al-4V titanium-alloy sheet and methods for estimating the minimum creep rate /

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...

Effects of creep stress on particulate aluminum-copper alloys /

Underwood, Ervin E., 1918-
Manning, G. K. (George K.)
Battelle Memorial Institute.

Prepared at Battelle Memorial Institute."September 1959."Cover title.Includes bibliographical refere...

Influence of various fabrication methods on the compressive strength of titanium skin-stringer panels /

Pride, Richard A. (Richard Allen), 1922-
Gardner, James E. (James Edward), 1942-
Royster, Dick M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Influence of fabrication methods on compressive strength of titanium alloy skin stringer panels.Prep...

Tensile properties of 6A1-4V titanium-alloy sheet under rapid-heatiing and constant-temperature conditions /

Price, Howard L.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Alloys, heat-resisting; Materials, Properties, tensile; Materials, Prope...

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 ...

Texture strengthening and fracture toughness of titanium alloy sheet at room and cryogenic temperatures /

Sullivan, Timothy L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 22-23).Mode of access: Internet

Tensile and creep properties of titanium-vanadium, titanium-molybdenum, and titanium-niobium /

Gray, Hugh R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9-10).Mode of ...

Hot-salt-stress-corrosion cracking and its effect on tensile properties of Ti-8Al-1Mo-1V titanium-alloy sheet /

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

Cover title."August 1968."Includes bibliographical references.Mode of access: Internet

Effect of initial loads and of moderately elevated temperature on the room-temperature fatigue life of Ti-8Al-1Mo-1V titanium-alloy sheet /

Imig, L.A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Strain-rate sensitivity of three titanium-alloy sheet materials after prolonged exposure at 550 ̊F (561 ̊K) [electronic resource] /

Baucom, Robert M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 10...

Smooth and sharpe-notch property variations for several heats of Ti-6A1-4V sheet at room and cryogenic temperatures Morgan P. Hanson and Hadley T. Richards.

Hanson, Morgan P.
Richards, Hadley T.
United States. National Aeronautics and Space Administration.

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

Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet /

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

Salt stress corrosion cracking effects on tensile and stress rupture properties of titanium alloy sh...

Residual-static-strength and slow-crack-growth behavior of duplex-annealed Ti-8Al-1Mo-1V sheet /

Figge, I. E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 13).Mode of access: Internet

A structural-efficiency evaluation of titanium at normal and elevated temperatures /

Heimerl, George J.
Barrett, Paul F.
United States. National Advisory Committee for Aeronautics.

January 1951

A structural-efficiency evaluation of titanium including comparisons with several other materials is...

A torsion creep tester for metals and alloys using electromechanical and servomechanical instrumentation /

Schwaneke, A. E.
Miller, V. R. (Vernon R.), 1941-
Nash, R. W. (Robert W.)
United States. Bureau of Mines.

"December 1970"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

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...

Effects of creep stress on particulate aluminum-copper alloys /

Underwood, Ervin E., 1918-
Manning, G. K. (George K.)
Battelle Memorial Institute.

Prepared at Battelle Memorial Institute."September 1959."Cover title.Includes bibliographical refere...

Influence of various fabrication methods on the compressive strength of titanium skin-stringer panels /

Pride, Richard A. (Richard Allen), 1922-
Gardner, James E. (James Edward), 1942-
Royster, Dick M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Influence of fabrication methods on compressive strength of titanium alloy skin stringer panels.Prep...

Tensile properties of 6A1-4V titanium-alloy sheet under rapid-heatiing and constant-temperature conditions /

Price, Howard L.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Alloys, heat-resisting; Materials, Properties, tensile; Materials, Prope...

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 ...

Texture strengthening and fracture toughness of titanium alloy sheet at room and cryogenic temperatures /

Sullivan, Timothy L.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 22-23).Mode of access: Internet

Tensile and creep properties of titanium-vanadium, titanium-molybdenum, and titanium-niobium /

Gray, Hugh R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9-10).Mode of ...

Hot-salt-stress-corrosion cracking and its effect on tensile properties of Ti-8Al-1Mo-1V titanium-alloy sheet /

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

Cover title."August 1968."Includes bibliographical references.Mode of access: Internet

Effect of initial loads and of moderately elevated temperature on the room-temperature fatigue life of Ti-8Al-1Mo-1V titanium-alloy sheet /

Imig, L.A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Strain-rate sensitivity of three titanium-alloy sheet materials after prolonged exposure at 550 ̊F (561 ̊K) [electronic resource] /

Baucom, Robert M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 10...

Smooth and sharpe-notch property variations for several heats of Ti-6A1-4V sheet at room and cryogenic temperatures Morgan P. Hanson and Hadley T. Richards.

Hanson, Morgan P.
Richards, Hadley T.
United States. National Aeronautics and Space Administration.

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

Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet /

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

Salt stress corrosion cracking effects on tensile and stress rupture properties of titanium alloy sh...

Residual-static-strength and slow-crack-growth behavior of duplex-annealed Ti-8Al-1Mo-1V sheet /

Figge, I. E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 13).Mode of access: Internet

A structural-efficiency evaluation of titanium at normal and elevated temperatures /

Heimerl, George J.
Barrett, Paul F.
United States. National Advisory Committee for Aeronautics.

January 1951

A structural-efficiency evaluation of titanium including comparisons with several other materials is...

A torsion creep tester for metals and alloys using electromechanical and servomechanical instrumentation /

Schwaneke, A. E.
Miller, V. R. (Vernon R.), 1941-
Nash, R. W. (Robert W.)
United States. Bureau of Mines.

"December 1970"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

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...

Effects of creep stress on particulate aluminum-copper alloys /

Underwood, Ervin E., 1918-
Manning, G. K. (George K.)
Battelle Memorial Institute.

Prepared at Battelle Memorial Institute."September 1959."Cover title.Includes bibliographical refere...

Influence of various fabrication methods on the compressive strength of titanium skin-stringer panels /

Pride, Richard A. (Richard Allen), 1922-
Gardner, James E. (James Edward), 1942-
Royster, Dick M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Influence of fabrication methods on compressive strength of titanium alloy skin stringer panels.Prep...

Tensile and compressive creep of 6al-4V titanium-alloy sheet and methods for estimating the minimum creep rate /

Abstract

Extracted data

Tensile and compressive creep of 6al-4V titanium-alloy sheet and methods for estimating the minimum creep rate /

Abstract

Extracted data

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