Books on the topic 'Crack damage'
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Carpinteri, Alberto. Mechanical damage and crack growth in concrete. Springer Netherlands, 1986. http://dx.doi.org/10.1007/978-94-009-4350-6.
Full textEllyin, Fernand. Fatigue Damage, Crack Growth and Life Prediction. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1509-1.
Full textEllyin, Fernand. Fatigue damage, crack growth, and life prediction. Chapman & Hall, 1997.
Find full textPete, Kantzos, Telesman Jack, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. National Aeronautics and Space Administration, 1995.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. AGARD, 1994.
Find full text1950-, Harris Charles E., and Langley Research Center, eds. Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCastelli, Michael G. Characterization of damage progression in SCS-6/Timetal 21S [0]₄ under thermomechanical fatigue loadings. National Aeronautics and Space Administration, 1994.
Find full textWanhill, R. J. H. Damage tolerance property comparisons for 2000 and 8000 series aluminium plate alloys. National Aerospace Laboratory, 1995.
Find full textC, Newman J., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Analysis and prediction of multiple-site damage (MSD) fatigue crack growth. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textC, Newman J., and Langley Research Center, eds. Methodology for predicting the onset of widespread fatigue damage in lap-splice joints. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCarpinteri, Alberto. Mechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer Netherlands, 1986.
Find full textCenter, Langley Research, ed. A progressive damage methodology for residual strength predictions of center-crack tension composite panels. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textNaik, Rajiv A. Observations of fatigue crack initiation and damage growth in notched titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textJozef Cornelis Walterus van Vroonhoven. Dynamic crack propagation in brittle materials: Analyses based on fracture and damage mechanics. Eindhoven University of Technology, 1996.
Find full textE, Harris C., Morris D. H, and Langley Research Center, eds. Surface crack analysis applied to impact damage in a thick graphite/epoxy composite. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textUnited States. National Aeronautics and Space Administration., ed. Damage mechanisms and controlled crack propagation in a hot pressed silicon nitride ceramic. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Damage mechanisms and controlled crack propagation in a hot pressed silicon nitride ceramic. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.
Find full textSchra, 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). National Aerospace Laboratory, 1992.
Find full textNorth 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. AGARD, 1994.
Find full textAdvisory 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. Agard, 1994.
Find full textA, Skinn D., Wright Laboratory (Wright-Patterson Air Force Base, Ohio). Materials Directorate., and Purdue University. Center for Information and Numerical Data Analysis and Synthesis., eds. Damage tolerant design handbook: A compilation of fracture and crack growth data for high-strength alloys. CINDAS, Purdue University, 1994.
Find full textC, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Computational simulation of damage progression of composite thin shells subjected to mechanical loads. National Aeronautics and Space Administration, 1996.
Find full textC, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Computational simulation of damage progression of composite thin shells subjected to mechanical loads. National Aeronautics and Space Administration, 1996.
Find full textE, Harris Charles, and United States. National Aeronautics and Space Administration., eds. Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue. National Aeronautics and Space Administration, 1995.
Find full textDore, Amanda Louise. Effects of fibre volume fraction on tensile damage and fatigue crack growth in Titanium metal matrix composites. University of Birmingham, 1997.
Find full textCenter, Langley Research, ed. Experimental verification of a progressive damage model for composite laminates based on continuum damage mechanics. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.
Find full textC, Driscoll R. M., Littlejohn G. S, Institution of Civil Engineers, and Building Research Establishment, eds. Has your house got cracks?: A homeowner's guide to subsidence and heave damage. 2nd ed. Institution of Civil Engineers and Building Research Establishment, 2002.
Find full textPiascik, Robert S. The characteristics of fatigue damage in the fuselage riveted lap splice joint. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textH, Starnes James, Newman J. C, and Langley Research Center, eds. Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textMechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. M. Nijhoff, 1986.
Find full textMechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer, 2011.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Surface Crack Analysis Applied to Impact Damage in a Thick Graphite-Epoxy Composite. Independently Published, 2018.
Find full textA progressive damage methodology for residual strength predictions of notched composite panels. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textEffects of Ballistic Impact Damage on Fatigue Crack Initiation in Ti- 6Al-4V Simulated Engine Blades. Storming Media, 2000.
Find full textManson, S. S., and G. R. Halford. Fatigue and Durability of Structural Materials. ASM International, 2006. http://dx.doi.org/10.31399/asm.tb.fdsm.9781627083447.
Full textLewis, Jaqueline. I Think I Have a Crack in My Amor! ... How'd That Happen?: Information to Help You Identify Your Triggers and How to Repair the Damage They Cause to Your Spiritual Armor. Independently Published, 2020.
Find full textLewis, Jaqueline. I Think I Have a Crack in My Armor! ... . How'd That Happen?: Information to Help You Identify Your Triggers and How to Repair the Damage They Cause to Your Spiritual Armor. Independently Published, 2020.
Find full textHas your House got Cracks?: A Homeowner's Guide to Subsidence and Heave Damage, 2nd edition. Thomas Telford Ltd, 2001. http://dx.doi.org/10.1680/hyhgc.30893.
Full textLittlejohn, G. S., R. M. C. Driscoll, and T. J. Freeman. Has Your House Got Cracks?: Second Edition: A Homeowner's Guide to Subsidence and Heave Damage. 2nd ed. Thomas Telford Services Ltd, 2003.
Find full textKemske, Bonnie. Kintsugi. Bloomsbury Publishing Plc, 2021. http://dx.doi.org/10.5040/9781789942743.
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