Books on the topic 'Fatigue tests'

Adamson, Daniel Edward Joseph. Fatigue tests of riveted bridge girders. Edmonton, Canada: University of Alberta, Dept. of Civil Engineering, 1995.

Schijve, J. The significance of flight simulation fatigue tests. Delft: Delft University of Technology, Dept. of Aerospace Engineering, 1985.

Lee, M. F. F/A-18 IFOSTP fatigue test airbag load determination on the vertical and horizontal tails. Melbourne: DSTO Aeronautical and Maritime Research Laboratory, 1995.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France 29th-30th September 1993. Neuilly sur Seine, France: AGARD, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. Neuilly sur Seine, France: AGARD, 1994.

Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting,, ed. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France, 29th-30th September 1993. Neuilly sur Seine: Agard, 1994.

J, De Luccia J., Russo M. T, and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. The fatigue in aircraft corrosion testing (FACT) programme. Neuilly sur Seine, France: AGARD, 1989.

Greenan, A. F. Constant amplitude fatigue tests on spot-welded mild steel joints. East Kilbride: National Engineering Laboratory, 1991.

Robin, Cook. Standard fatigue test specimens for fastener evaluation. Neuilly sur Seine, France: AGARD, 1987.

Willard, Scott A. A record of all marker bands found in the upper rivet rows of 2 adjacent bays from a fuselage lap splice joint. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

A, Clevenson Sherman, and Langley Research Center, eds. High intensity acoustic tests of a thermally stressed aluminum plate in tafa. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Leeuwen, H. P. van. Automated measurement of crack length and load line displacement at elevated temperature. Neuilly sur Seine, France: AGARD, 1988.

T, Shimski John, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology., eds. Evaluation of advanced lubricants for aircraft applications using gear surface fatigue tests. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

1931-, Fisher John W., American Association of State Highway and Transportation Officials., and United States. Federal Highway Administration., eds. Evaluation of fatigue tests and design criteria on welded details. Washington, D.C: Transportation Research Board, National Research Council, 1986.

Have, A. A. ten. WISPER and WISPERX: Final definition of two standardised fatigue loading sequences for wind turbine blades. Amsterdam: National Aerospace Laboratory, 1992.

Have, A. A. ten. WISPER and WISPERX: Final definition of two standardised fatigue loading sequences for wind turbine blades. Amsterdam: National Aerospace Laboratory, 1992.

E, Shapiro D., and United States. Bureau of Mines, eds. Bending fatique tests on flattened strand wire rope at high working loads. [Washington, D.C.?]: U.S. Dept. of Interior, Bureau of Mines, 1995.

E, Shapiro D., and United States. Bureau of Mines., eds. Bending fatigue tests on flattened strand wire rope at high working loads. [Washington, D.C.?]: U.S. Dept. of Interior, Bureau of Mines, 1995.

Sreeramesh, Kalluri, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Elevated temperature axial and torsional fatigue behavior of Haynes 188. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Miyoshi, Kazuhisa. Preliminary study on fatigue strengths of fretted Ti-48Al-2Cr-2Nb. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Miyoshi, Kazuhisa. Preliminary study on fatigue strengths of fretted Ti-48Al-2Cr-2Nb. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

D, Raizenne M., and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. AGARD engine disc cooperative test programme. Neuilly sur Seine, France: AGARD, 1988.

W. G. J. 't Hart. Fatigue damage in composites under different loading conditions. Amsterdam: National Aerospace Laboratory, 1988.

W, Smith Stephen. The effect of O₂, H₂O, and N₂ on the fatigue crack growth behavior of an Ü + Ý titanium alloy at 24C̊ and 177C̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

D, Noebe R., and United States. National Aeronautics and Space Administration., eds. Low cycle fatigue behavior of polycrystalline NiAl at 300 and 1000K. [Washington, DC]: National Aeronautics and Space Administration, 1993.

D, Noebe Ronald, and United States. National Aeronautics and Space Administration., eds. Low cycle fatigue behavior of polycrystalline NiAl at 300 and 1000K. [Washington, DC]: National Aeronautics and Space Administration, 1993.

W, Smith Stephen. The effect of Ob2s, Hb2sO, and Nb2s on the fatigue crack growth behavior of an gas + gbs titanium alloy at 24C and 177C. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. AGARD engine disc cooperative test programme. Neuilly sur Seine, France: AGARD, 1993.

Castelli, Michael G. Isothermal damage and fatigue behavior and SCS-6/timetal 21S [0/90]s composite at 650C̊. [Washington, DC]: National Aeronautics and Space Administration, 1994.

W. G. J. 't Hart. Delamination growth in improved carbon composites under constant amplitude fatigue loading. Amsterdam, Netherlands: National Aerospace Laboratory, 1989.

Wanhill, R. J. H. Corrosion fatigue crack arrest in aluminium alloys: Basic data. Amsterdam: National Aerospace Laboratory, 1987.

Schra, L. Influence of gust spectrum variations on fatigue crack growth behaviour of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 4). Amsterdam: National Aerospace Laboratory, 1992.

Collins, William Edward. Effects of sleep loss on vestibular response during simple and complex vestibular stimulation. Washington, D.C: U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Medicine, 1986.

Gerharz, J. J. Standardized environmental fatigue sequence for the evaluation of composite components in combat aircraft (ENSTAFF = ENvironmental FalSTAFF). Amsterdam: National Aerospace Laboratory, 1987.

Webb, G. L. Thermal fatigue tests of a radiative heat shield panel for a hypersonic transport. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Spahl, Robert. Safety tests for components of vehicles using load spectra. Aachen: Shaker, 1996.

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. [Washington, DC]: National Aeronautics and Space Administration, 1996.

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. [Washington, DC]: National Aeronautics and Space Administration, 1996.

1960-, Bonacuse Peter J., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. An axial-torsional, thermomechanical fatigue testing technique. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Alan, Turza, Chaplin Mike, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. The surface fatigue life of contour induction hardened AISI 1552 gears. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Center, Lewis Research, ed. An evaluation of the plasticity-induced crack-closure. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Alan, Turza, Chaplin Mike, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. The surface fatigue life of contour induction hardened AISI 1552 gears. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Center, Langley Research, ed. Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, ed. Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

P, Campion R., and United States. National Aeronautics and Space Administration., eds. Mechanical and physical properties of both unaged and aged Coflon and Tefzel: CAPP, international research project on the effects of chemical ageing of polymers on performance properties. Austin, Tex: Texas Research Institute, 1996.

P, Campion R., and United States. National Aeronautics and Space Administration., eds. Mechanical and physical properties of both unaged and aged Coflon and Tefzel: CAPP, international research project on the effects of chemical ageing of polymers on performance properties. Austin, Tex: Texas Research Institute, 1996.

Smith, Stephen W. Simulation of fatigue crack initiation at corrosion pits with EDM notches. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

W, Smith Stephen. Simulation of fatigue crack initiation at corrosion pits with EDM notches. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

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.