Titanium-aluminum-vanadium alloys -- Ductility
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Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet (National Aeronautics and Space Administration ;, 1969), by Dick M. Royster, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
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Filed under: Titanium-aluminum-vanadium alloys- Oxidation characteristics of Ti-25Al-10Nb-3V-1Mo intermetallic alloy (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Terryl A. Wallace and Langley Research Center (page images at HathiTrust)
- Friction and wear of titanium alloys and copper alloys sliding against titanium - 6-percent-aluminum - 4-percent-vanadium alloy in air at 430C̊ (U.S. National Aeronautics and Space Administration ;, 1976), by Donald W. Wisander, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Selected fretting-wear-resistant coatings for titanium--6-percent-aluminum--4-percent-vanadium alloy (U.S. National Aeronautics and Space Administration ;, 1976), by Robert C. Bill, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Equipment and procedures for glass-bead peening titanium-alloy tanks (National Aeronautics and Space Administration ;, 1968), by Thomas T. Bales, W. Barry Lisagor, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Growth of surface and corner cracks in beta-processed and mill-annealed Ti-6Al-4V (National Aeronautics and Space Administration ;, 1975), by Paul D. Bell and Langley Research Center (page images at HathiTrust)
- Some factors affecting the stress-corrosion cracking of Ti-6Al-4V alloy in methanol (National Aeronautics and Space Administration ;, 1969), by W. Barry Lisagor, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet (National Aeronautics and Space Administration ;, 1969), by Dick M. Royster, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide (National Aeronautics and Space Administration ;, 1968), by W. Barry Lisagor, Thomas T. Bales, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Crack-closure and crack-growth measurements in surface-flawed titanium alloy Ti-6Al-4V (National Aeronautics and Space Administration ;, 1975), by Elber Wolf and Langley Research Center (page images at HathiTrust)
- Salt stress corrosion of residually stressed Ti-8Al-1Mo-1V alloy sheet after exposure at elevated temperatures (National Aeronautics and Space Administration ;, 1966), by Howard B. Dexter and Langley Research Center (page images at HathiTrust)
- Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide (National Aeronautics and Space Administration ;, 1968), by W. Barry Lisagor, Thomas T. Bales, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide (National Aeronautics and Space Administration ;, 1968), by W. Barry Lisagor, Thomas T. Bales, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Effect of outdoor exposure at ambient and elevated temperatures on fatigue life of Ti-6Al-4V titanium alloy sheet in the annealed and the solution-treated and aged condition (National Aeronautics and Space Administration ;, 1974), by Edward P. Phillips and Langley Research Center (page images at HathiTrust)
- Load interaction effects on fatigue crack growth in Ti-6Al-4V alloy (National Aeronautics and Space Administration ;, 1973), by Robert Peh-ying Wei, J. H. FitzGerald, T. T. Shih, Langley Research Center, and Lehigh University (page images at HathiTrust)
- A study of crack closure in fatigue (National Aeronautics and Space Administration ;, 1973), by T. T. Shih, Robert Peh-ying Wei, Langley Research Center, and Lehigh University (page images at HathiTrust)
- Fatigue-test acceleration with flight-by-flight loading and heating to simulate supersonic-transport operation (National Aeronautics and Space Administration ;, 1973), by L. A. Imig, L. E. Garrett, and Langley Research Center (page images at HathiTrust)
- Effect of outdoor exposure at ambient and elevated temperatures on fatigue life of Ti-6Al-4V titanium alloy sheet in the annealed and the solution-treated and aged condition (National Aeronautics and Space Administration ;, 1974), by Edward P. Phillips and Langley Research Center (page images at HathiTrust)
- Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet (National Aeronautics and Space Administration ;, 1969), by Dick M. Royster, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Effect of outdoor exposure at ambient and elevated temperatures on fatigue life of Ti-6Al-4V titanium alloy sheet in the annealed and the solution-treated and aged condition (National Aeronautics and Space Administration ;, 1974), by Edward P. Phillips and Langley Research Center (page images at HathiTrust)
- Soft body impact damage effects on boron-aluminum composites (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1975., 1975), by William J. Jaques and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
- Ti-6A1-4V alloy castings prepared in zircon sand molds and the effect of hot isostatic pressing (U.S. Dept. of the Interior, Bureau of Mines, 1984), by J. I. Paige, Jack L. Henry, and P. G. Clites (page images at HathiTrust)
- Equipment and procedures for glass-bead peening titanium-alloy tanks (National Aeronautics and Space Administration ;, 1968), by Thomas T. Bales, W. Barry Lisagor, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Some factors affecting the stress-corrosion cracking of Ti-6Al-4V alloy in methanol (National Aeronautics and Space Administration ;, 1969), by W. Barry Lisagor, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Hot-salt-stress-corrosion cracking and its effect on tensile and stress-rupture properties of Ti-6Al-4V titanium-alloy sheet (National Aeronautics and Space Administration ;, 1969), by Dick M. Royster, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide (National Aeronautics and Space Administration ;, 1968), by W. Barry Lisagor, Thomas T. Bales, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
- Coatings and surface treatments for longtime protection of Ti-8Al-1Mo-1V alloy sheet from hot-salt stress corrosion (National Aeronautics and Space Administration ;, 1968), by Bland A. Stein, Dick M. Royster, H. Benson Dexter, and Langley Research Center (page images at HathiTrust)
- The stress corrosion susceptibility of several alloys in hydrazine fuels (National Aeronautics and Space Administration ;, 1974), by William Gilbreath, Michael J. Adamson, and Ames Research Center (page images at HathiTrust)
- Salt stress corrosion of residually stressed Ti-8Al-1Mo-1V alloy sheet after exposure at elevated temperatures (National Aeronautics and Space Administration ;, 1966), by Howard B. Dexter and Langley Research Center (page images at HathiTrust)
- Crack-closure and crack-growth measurements in surface-flawed titanium alloy Ti-6Al-4V (National Aeronautics and Space Administration ;, 1975), by Elber Wolf and Langley Research Center (page images at HathiTrust)
- Hot press and roll welding of titanium-6-percent-aluminum-4-percent-vanadium bar and sheet with auto-vacuum cleaning (National Aeronautics and Space Administration ;, 1972), by Kenneth H. Holko and Lewis Research Center (page images at HathiTrust)
- Development of the weld-braze joining process (National Aeronautics and Space Administration ;, 1973), by Thomas T. Bales, Winfrey E. Arnold, Dick M. Royster, and Langley Research Center (page images at HathiTrust)
- Hot press and roll welding of titanium-6-percent-aluminum-4-percent-vanadium bar and sheet with auto-vacuum cleaning (National Aeronautics and Space Administration ;, 1972), by Kenneth H. Holko and Lewis Research Center (page images at HathiTrust)
- Salt stress corrosion of residually stressed Ti-8Al-1Mo-1V alloy sheet after exposure at elevated temperatures (National Aeronautics and Space Administration ;, 1966), by Howard B. Dexter and Langley Research Center (page images at HathiTrust)
- Salt stress corrosion of residually stressed Ti-8Al-1Mo-1V alloy sheet after exposure at elevated temperatures (National Aeronautics and Space Administration ;, 1966), by Howard B. Dexter and Langley Research Center (page images at HathiTrust)
- Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys (National Aeronautics and Space Administration ;, 1975), by Richard A. Everett and Langley Research Center (page images at HathiTrust)
- Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) (National Aeronautics and Space Administration ;, 1969), by Dick M. Royster, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Flaw growth behavior in thick welded plates of 2219-T87 aluminum at room and cryogenic temperatures (National Aeronautics and Space Administration ;, 1973), by Royce G. Forman, James D. Medlock, Samuel V. Glorioso, United States National Aeronautics and Space Administration, and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Factors affecting the ductility of iron-chromium-aluminum alloy sheet (Battelle Memorial Institute ;, 1960), by Roy W. Endebrock, Ronald F. Dickerson, Ellis L. Foster, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
- Tensile and creep properties of titanium-vanadium, titanium-molybdenum, and titanium-niobium (National Aeronautics and Space Administration ;, 1975), by Hugh R. Gray and Lewis Research Center (page images at HathiTrust)
- Strain-rate sensitivity of three titanium-alloy sheet materials after prolonged exposure at 550 ̊F (561 ̊K) (National Aeronautics and Space Administration ;, 1969), by Robert M. Baucom, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Hot-salt stress-corrosion of titanium alloys : generation of hydrogen and its embrittling effect (National Aeronautics and Space Administration ;, 1969), by Hugh R. Gray, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Tensile properties to 650 ̊C and deformation structures in a precipitation-strengthened titanium-aluminum alloy (National Aeronautics and Space Administration ;, 1973), by Madan G. Mendiratta, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Effect of nuclear radiation at cryogenic temperatures on the tensile properties of titanium and titanium-base alloys (National Aeronautics and Space Administration ;, 1969), by Charles L. Younger, Fred A. Haley, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Exploratory study of elevated-temperature tensile properties of alloys based on the intermetallic compound TiNi (National Aeronautics and Space Administration ;, 1974), by Marvin Garfinkle and Lewis Research Center (page images at HathiTrust)
- NASA TN D-6309 (National Aeronautics and Space Administration ;, 1971), by Gary R. Halford, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- An investigation of hot ductility of inconel and inconel x (Oak Ridge National Laboratory, 1958), by Edward A. Pigan and U.S. Atomic Energy Commission (page images at HathiTrust)
- Influence of several metallurgical variables on the tensile properties of hastelloy N (Oak Ridge National Laboratory, 1964), by H. E. McCoy and U.S. Atomic Energy Commission (page images at HathiTrust)
- Instrumental impact and residual tensile strength testing of eight-ply carbon/epoxy specimens (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by A. T. Nettles and George C. Marshall Space Flight Center (page images at HathiTrust)
- Comparison of polyester, film-yarn composite, balloon materials subjected to shear and biaxial loading (National Aeronautics and Space Administration ;, 1972), by R. J. Niccum, Langley Research Center, and G.T. Schjeldahl Company (page images at HathiTrust)
- Refractory metal valves for 1900 deg F service in alkali metal systems (National Aeronautics and Space Administration ;, 1971), by R. W. Harrison, J. Holowach, Lewis Research Center, and General Electric Company (page images at HathiTrust)
- Thermal fatigue of ductile materials. III, Behavior of crucible 422 steel (National Aeronautics and Space Administration, 1959), by Francis J. Clauss and Lewis Research Center (page images at HathiTrust)
- Ductile ceramics. I, Factors affecting the plasticity of sodium chloride, lithium fluoride, and magnesium oxide single crystals (National Aeronautics and Space Administration, 1959), by Carl A. Stearns, Robert A. Lad, Ann E. Pack, and Lewis Research Center (page images at HathiTrust)
- Ductile ceramics. II, Introductory study of ductility in polycrystalline sodium chloride and magnesium oxide (National Aeronautics and Space Administration, 1959), by Charles E. May, Robert A. Lad, Hubert H. Grimes, and Lewis Research Center (page images at HathiTrust)
- Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight (National Aeronautics and Space Administration, 1962), by Kenneth W. Goodson, Kalman J. Grunwald, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Vacuum-induction, vacuum-arc, and air-induction melting of a complex heat-resistant alloy (National Aeronautics and Space Administration, 1959), by Raymond Frank Decker, J. W. Freeman, John P. Rowe, and University of Michigan (page images at HathiTrust)
- On the ductile enlargement of voids in triaxial stress fields (Division of Engineering, Brown University, 1968), by J. R. Rice, D. M. Tracey, U.S. Atomic Energy Commission, and Brown University. Division of Engineering (page images at HathiTrust)
- Strain-hardening and interaction effects on the growth of voids in ductile fracture (Division of Engineering, Brown University, 1968), by D. M. Tracey, U.S. Atomic Energy Commission, and Brown University. Division of Engineering (page images at HathiTrust)
- Significant issues in proof testing : a critical appraisal (National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994), by G. G. Chell and George C. Marshall Space Flight Center (page images at HathiTrust)
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