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Nickel-titanium alloys -- Testing

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• Nickel-titanium alloys
• Nickel alloys -- Testing
• Titanium alloys -- Testing
• Testing

• 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)

Items below (if any) are from related and broader terms.

• Continuous-band nitinol heat engine : final report (The Department, 1980), by Energy Research Associates and United States. Department of Energy. Region IX. (page images at HathiTrust)
• A tentative titanium-nickel diagram (U.S. Dept. of the Interior, Bureau of Mines, 1949), by C. E. Armantrout, D. C. Root, E. T. Hayes, and J. R. Long (page images at HathiTrust)
• The properties of TiNi and associated phases (United States Naval Ordnance Laboratory, 1961), by W. J Buehler, R. C Wiley, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• 55-Nitinol--the alloy with a memory: its physical metallurgy, properties, and applications; a report (Technology Utilization Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1972), by Curtis M. Jackson, Roman Jerzy Wasilewski, H. J. Wagner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The development of melting and casting procedures for nitinol nickel-base alloys (Battelle Memorial Institute, 1968), by David C. Drennen, H. J. Wagner, C. M. Jackson, U.S. Atomic Energy Commission, and Sandia Laboratories (page images at HathiTrust)
• Nitinol self-descaling surface for geothermal scale control (Berkeley, California : Lawrence Berkeley Laboratory, University of California, 1977., 1977), by Oleh Weres, Lawrence Berkeley Laboratory. Energy and Environment Division, and United States. Energy Research and Development Administration (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)

• Investigation of the strengthening mechanisms of dispersion-strengthened alloys. Part II (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Richard J. Murphy, Nicholas J. Grant, Varadachari Sadagopan, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Department of Metallurgy (page images at HathiTrust)
• Investigation of the strengthening mechanisms of dispersion-strengthened alloys. Part II (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Richard J. Murphy, Nicholas J. Grant, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Department of Metallurgy (page images at HathiTrust)

• The mechanical properties of INOR-8 (Oak Ridge National Laboratory, 1961), by R. W. Swindeman, U.S. Atomic Energy Commission, Union Carbide Corporation, and Oak Ridge National Laboratory. Metallurgy Division (page images at HathiTrust)
• Effects of alloy composition on cyclic flame hot-corrosion attack of cast nickel-base superalloys at 900⁰C (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Daniel L. Deadmore and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Application of directional solidification to a NASA nickel- base alloy (TAZ-8B) (National Aeronautics and Space Administration ;, 1968), by John C. Freche, Richard L. Ashbrook, William J. Waters, and Lewis Research Center (page images at HathiTrust)
• Effects of silicon additions on oxidation and mechanical behavior of the nickel-base superalloy B-1900 (National Aeronautics and Space Administration, 1975), by Robert V. Miner and Carl E. Lowell (page images at HathiTrust)
• Creep and tensile properties of several oxide-dispersion-strengthened nickel-base alloys at 1365 K (National Aeronautics and Space Administration ;, 1977), by J. Daniel Whittenberger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Refractory-metal-fiber-nickel-base-alloy composites for use at high temperatures (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Donald W. Petrasek, John W. Weeton, and Robert A. Signorelli (page images at HathiTrust; US access only)
• Susceptibility to hot corrosion of four nickel-base superalloys NASA-TRW VIA, B-1900, 713C, and IN-738 (National Aeronautics and Space Administration ;, 1977), by Carl A. Stearns, George C. Fryburg, Fred J. Kohl, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Friction and wear under fretting conditions of materials for use as wire friction dampers of compressor blade vibration (National Aeronautics and Space Administration ;, 1968), by Max A. Swikert, Robert L. Johnson, and Lewis Research Center (page images at HathiTrust)
• Effect of cyclic conditions on the dynamic oxidation of gas turbine superalloys (National Aeronautics and Space Administration ;, 1974), by James R. Johnston, Richard L. Ashbrook, and Lewis Research Center (page images at HathiTrust)
• Comparison of isothermal and cyclic oxidation behavior of twenty-five commercial sheet alloys at 1150 ̊C (National Aeronautics and Space Administration ;, 1974), by Charles A. Barrett, Carl E. Lowell, and Lewis Research Center (page images at HathiTrust)
• Evaluation of alloys and coatings for use in automobile thermal reactors (National Aeronautics and Space Administration ;, 1974), by Charles P. Blankenship, Robert E. Oldrieve, and Lewis Research Center (page images at HathiTrust)
• Stress-rupture strength and microstructural stability of tungsten-hafnium-carbon-wire-reinforced superalloy composites (National Aeronautics and Space Administration ;, 1974), by Donald W. Petrasek, Robert A. Sigorelli, and Lewis Research Center (page images at HathiTrust)
• Metallographic and x-ray study of nickel alloys of 20 - 33 percent molybdenum. (Technical Information Extension, 1955), by Donald W. Stoffel (page images at HathiTrust)
• Development of a nickel base alloy sheet for high temperature application (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by H. Greenewald, Terrence J. Riley, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and Chance Vought Corporation (page images at HathiTrust)

• An evaluation of nickel-copper alloys for use as graphite-cladding materials at elevated temperatures (Technical Services, Department of Commerce ;, 1960), by J. C. Bokros, United States Maritime Administration, U.S. Atomic Energy Commission, and General Dynamics Corporation. General Atomic Division (page images at HathiTrust)

• Tensile tests on invar sheet at cryogenic temperatures (Los Alamos Scientific Laboratory of the University of California, 1965), by David T. Eash, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)

• A study of nickel-iron and nickel krupp metal thermoelements (1912), by Walter Boatman Worsham (page images at HathiTrust; US access only)

• Preliminary evaluation of tungsten alloy fiber-nickel-base alloy composites for turbojet engine applications (National Aeronautics and Space Administration ;, 1970), by Donald W. Petrasek, Robert A. Signorelli, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

• An Analytic and experimental evaluation of flowing air test conditions for selected metallics in a shuttle TPS application (National Aeronautics and Space Administration ;, 1975), by John W. Schaefer, Langley Research Center, and Acurex Corporation. Aerotherm Division (page images at HathiTrust)
• An improved diffusion welding technique for TD-NiCR sheet (National Aeronautics and Space Administration ;, 1973), by Kenneth H. Holko and Lewis Research Center (page images at HathiTrust)

• Calculation of thermal-fatigue life based on accumulated creep damage (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1969), by David A. Spera (page images at HathiTrust; US access only)

• Effects of composition and processing variables on transverse rupture strength and hardness of nickel-alloy-bonded titanium carbide (U.S. Dept. of the Interior, Bureau of Mines, 1987), by G. T. Fisher, Gene Asai, and L. L. Oden (page images at HathiTrust)

• Fatigue studies of inor-8 (Battelle Memorial Institute ;, 1959), by Raymond G. Carlson, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)

• Oxidation of nickel- and cobalt-base superalloys (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1965., 1965), by Carl H. Lund, H. J. Wagner, Defense Metals Information Center (U.S.), United States. Air Force. Systems Command. Research and Technology Division, and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)

• Mechanical properties of diffusion-bonded titanium sandwich constructions (Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1973), by Edward W. Kuenzi and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Nondestructive testing techniques for titanium billets. (Air Force Materials Laboratory, Air Force Systems Command, 1969), by Frank J. Sattler (page images at HathiTrust)
• Effect of LID® processing on the microstructure and mechanical properties of Ti-6Al-4V and Ti-6Al-2Sn-4Zr-2Mo titanium foil-gauge materials (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Linda B. Blackburn and Langley Research Center (page images at HathiTrust)
• Emittance, catalysis, and dynamic oxidation of Ti-14Al-21Nb (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by K. E. Wiedemann, Sankara Narayan Sankaran, R. K. Clark, and Langley Research Center (page images at HathiTrust)
• Influence of various fabrication methods on the compressive strength of titanium skin-stringer panels (National Aeronautics and Space Administration ;, 1969), by Richard A. Pride, James E. Gardner, Dick M. Royster, United States National Aeronautics and Space Administration, and Langley 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)
• Metallurgical and mechanical characteristics of high-purity Titanium-base alloys (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1960., 1960), by Richard W. Douglass, Robert I. Jaffee, Horace R. Ogden, Frank C. Holden, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Battelle Memorial Institute (page images at HathiTrust)
• Metallurgical and mechanical characteristics of high-purity Titanium-base alloys (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Albert G. Imgram, Robert I. Jaffee, Horace R. Ogden, Richard A. Wood, Dean N. Williams, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Battelle Memorial Institute (page images at HathiTrust)
• Extended study of flaw growth at fastener holes. Volume 2, Data tabulation (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978), by T. M. Hsu, W. M. McGee, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Evaluation of the reliability and sensitivity of NDT methods for titanium alloys (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1973., 1973), by Robert J. Lord, Air Force Materials Laboratory (U.S.), McDonnell Aircraft Company, and McDonnell Douglas Corporation (page images at HathiTrust)
• Extended study of flaw growth at fastener holes. Volume 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), by T. M. Hsu, J. A. Aberson, W. M. McGee, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Evaluation of the reliability and sensitivity of NDT methods for titanium alloys. Volume II (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1974., 1974), by Robert J. Lord, Air Force Materials Laboratory (U.S.), McDonnell Aircraft Company, and McDonnell Douglas Corporation (page images at HathiTrust)

• NASA TN D-4061 (National Aeronautics and Space Administration ;, 1967), by L.A. Imig, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Effects of longtime environmental exposure on mechanical properties of sheet materials for a supersonic transport (National Aeronautics and Space Administration ;, 1968), by Richard A. Pride 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)

• NASA TN D-4444 (National Aeronautics and Space Administration ;, 1968), by Timothy L. Sullivan, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determination of design data for heat treated titanium alloy sheet. Volume 2b, Test techniques and results for creep and fatigue (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by D. L. White, H. T. Watson, United States. Air Force. Systems Command. Aeronautical Systems Division, and Lockheed-Georgia Company (page images at HathiTrust)

More items available under broader and related terms at left.