Books on the topic 'Cyclic tests'

Lade, P. Cyclic triaxial tests of the Bootlegger Cove Formation, Anchorage, Alaska. [Washington, D.C.]: U.S. G.P.O., 1988.

Lade, P. Cyclic triaxial tests of the Bootlegger Cove Formation, Anchorage, Alaska. Washington, DC: Dept. of the Interior, 1988.

Ahmed, Rafiq. Cyclic loads tests of carbon involute solid rocket motor outer boot ring segments. Huntsville, Ala: Marshall Space Flight Center, 1988.

Ahmad, Rafiq. Cyclic loads tests of carbon involute solid rocket motor outer boot ring segments. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Molenkamp, F. Numerical simulation of cyclic triaxal tests by means of the constitutive model ALTERNAT. Manchester: University of Manchester, 1989.

United States. National Aeronautics and Space Administration., ed. Rhenium material properties. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Wilkinson, C. High temperature cyclic behaviour of aerospace materials: room temperature validation tests of Ti-6Al-4V. Neuilly sur Seine, France: AGARD, 1994.

United States. National Aeronautics and Space Administration., ed. The effect of laser glazing on life of ZrO TBC's in cyclic burner rig tests. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Mann, J. Y. Influence of hole surface finish, cyclic frequency and spectrum severity on the fatigue behaviour of thick section aluminium alloy pin joints (U). Melbourne, Victoria: Aeronautical Research Laboratory, 1987.

United States. National Aeronautics and Space Administration., ed. 10,000-hour cyclic oxidation behavior at 982 C (1800 F) of 68 high-temperature Co, Fe-, and Ni-base alloys. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. 10,000-hour cyclic oxidation behavior at 982 C (1800 F) of 68 high-temperature Co, Fe-, and Ni-base alloys. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. 10,000-hour cyclic oxidation behavior at 982 C (1800 F) of 68 high-temperature Co, Fe-, and Ni-base alloys. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Rivers, H. Kevin. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Wilkinson, C. Structures and Materials Panel Working Group 26 on High temperature cyclic behaviour of aerospace materials: Room temperature validation tests of Ti-6AI-4V. Neuilly sur Seine: Agard, 1994.

J, Ayton C., ed. Triumph twins from 1937: Road tests and features from theMotor cycle & Motor cycling. Bideford: Bay View Books, 1990.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Center, Lewis Research, ed. Characterization and cycle tests of lightweight nickel electrodes. Cleveland, Ohio: Lewis Research Center, 1989.

Britton, Doris L. Characterization and cycle tests of lightweight nickel electrodes. Cleveland, Ohio: Lewis Research Center, 1989.

Boschen, John F. Tests of the relation between money and output in the real business cycle model. [Philadelphia]: Federal Reserve Bank of Philadelphia, 1987.

Focused assessment: Enriching the instructional cycle. Bloomington, IN: Solution Tree, 2008.

V, Lorenz Gary, and United States. National Aeronautics and Space Administration., eds. RE-1000 free-piston Stirling engine sensitivity test results. [Washington, DC: National Aeronautics and Space Administration, 1986.

V, Lorenz Gary, and United States. National Aeronautics and Space Administration., eds. RE-1000 free-piston Stirling engine sensitivity test results. [Washington, DC: National Aeronautics and Space Administration, 1986.

V, Lorenz Gary, and United States. National Aeronautics and Space Administration., eds. RE-1000 free-piston Stirling engine sensitivity test results. [Washington, DC: National Aeronautics and Space Administration, 1986.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Cataldo, Robert L. Parametric and cycle tests of a 40-A-hr bipolar nickel-hydrogen battery. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

G, Fox Alan. The influence of TIG welding thermal cycles on HSLA-100 steel plate. Monterey, Calif: Naval Postgraduate School, 1993.

United States. National Aeronautics and Space Administration., ed. Options for flight testing rocket-based combined-cycle (RBCC) engines. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

Anhalt, István. Thisness: A duo-drama cycle for mezzo-soprano and accompanist. [Toronto?]: The author, 1985.

M, Manderscheid J., and Lewis Research Center, eds. Simplified cyclic structural analyses of SSME turbine blades. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Martz, Geoff. Cracking the GMAT with sample tests on CD-ROM. 2nd ed. New York: Random House, 2002.

Miller, Ross. Assessment in cycles of improvement: Faculty designs for essential learning outcomes. Washington, D.C: Association of American Colleges and Universities, 2007.

Todd, Stanley, and Moore Elizabeth, eds. Short-cycle assessment: Improving student achievement through formative assessment. Larchmont, NY: Eye On Education, 2008.

Stubbe, E. J. Assessment study of RELAP5/MOD2 cycle 36.04 based on pressurizer safety and relief valve tests. Washington, DC: Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1990.

United States. National Aeronautics and Space Administration., ed. Report for period ending July 31, 1985 ... entitled Characterization of the relationship of the cure cycle chemistry to cure cycle processing properties. Williamsburg, Va: College of William and Mary, Dept. of Chemistry, 1985.

(Firm), Aerojet, and United States. National Aeronautics and Space Administration., eds. Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08: Contract no. NAS 5-32314. [Washington, DC: National Aeronautics and Space Administration, 1998.

(Firm), Aerojet, and United States. National Aeronautics and Space Administration., eds. Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08: Contract no. NAS 5-32314. [Washington, DC: National Aeronautics and Space Administration, 1998.

A, Scheiman David, and United States. National Aeronautics and Space Administration., eds. Thermal cycling of Mir Cooperative Solar Array (MCSA) test panels. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Christiane, Brusselmans, and Catholic Church, eds. Sunday: The book of readings, cycle C. Mill Hill, England: T. Shand Publications, 1989.

Graciously hear us: General intercessions for cycles A, B & C. Notre Dame, Ind: Ave Maria Press, 1998.

Payne, Richard E. Long-term tests of some inexpensive barometers and results of pressure cycling of an AIR-DB-1A. Woods Hole, Mass: Upper Ocean Processes Group, Woods Hole Oceanographic Institution, 1994.

Payne, Richard E. Long-term tests of some inexpensive barometers and results of pressure cycling of an AIR-DB-1A. Woods Hole, Mass: Upper Ocean Processes Group, Woods Hole Oceanographic Institution, 1994.

A, Miller Robert, and Lewis Research Center, eds. Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.