Книги з теми "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.
Повний текст джерелаEllyin, Fernand. Fatigue Damage, Crack Growth and Life Prediction. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1509-1.
Повний текст джерелаEllyin, Fernand. Fatigue damage, crack growth, and life prediction. Chapman & Hall, 1997.
Знайти повний текст джерелаPete, 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.
Знайти повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. AGARD, 1994.
Знайти повний текст джерела1950-, 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.
Знайти повний текст джерелаCastelli, Michael G. Characterization of damage progression in SCS-6/Timetal 21S [0]₄ under thermomechanical fatigue loadings. National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаWanhill, R. J. H. Damage tolerance property comparisons for 2000 and 8000 series aluminium plate alloys. National Aerospace Laboratory, 1995.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаCarpinteri, Alberto. Mechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer Netherlands, 1986.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаNaik, Rajiv A. Observations of fatigue crack initiation and damage growth in notched titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаJozef Cornelis Walterus van Vroonhoven. Dynamic crack propagation in brittle materials: Analyses based on fracture and damage mechanics. Eindhoven University of Technology, 1996.
Знайти повний текст джерелаE, 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаSchra, 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.
Знайти повний текст джерелаNorth 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.
Знайти повний текст джерелаAdvisory 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.
Знайти повний текст джерелаA, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаE, 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.
Знайти повний текст джерелаDore, Amanda Louise. Effects of fibre volume fraction on tensile damage and fatigue crack growth in Titanium metal matrix composites. University of Birmingham, 1997.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаC, 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.
Знайти повний текст джерелаPiascik, Robert S. The characteristics of fatigue damage in the fuselage riveted lap splice joint. National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаH, 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.
Знайти повний текст джерелаFatigue Damage, Crack Growth and Life Prediction. Springer Netherlands, 1996.
Знайти повний текст джерелаMechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. M. Nijhoff, 1986.
Знайти повний текст джерелаMechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer, 2011.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Surface Crack Analysis Applied to Impact Damage in a Thick Graphite-Epoxy Composite. Independently Published, 2018.
Знайти повний текст джерелаA progressive damage methodology for residual strength predictions of notched composite panels. National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаEffects of Ballistic Impact Damage on Fatigue Crack Initiation in Ti- 6Al-4V Simulated Engine Blades. Storming Media, 2000.
Знайти повний текст джерелаManson, 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.
Повний текст джерелаLewis, 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.
Знайти повний текст джерелаLewis, 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.
Знайти повний текст джерелаKent, Gordon. Damage Control. HarperCollins Publishers Limited, 2005.
Знайти повний текст джерелаKent, Gordon. Damage Control. HarperCollins Publishers Limited, 2010.
Знайти повний текст джерелаHas 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.
Повний текст джерелаLittlejohn, 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.
Знайти повний текст джерелаKemske, Bonnie. Kintsugi. Bloomsbury Publishing Plc, 2021. http://dx.doi.org/10.5040/9781789942743.
Повний текст джерела