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1

Chona, R., and WR Corwin, eds. Rapid Load Fracture Testing. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1992. http://dx.doi.org/10.1520/stp1130-eb.

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2

Wanhill, R. J. H. Spacecraft sustained load fracture control. Amsterdam: National Aerospace Laboratory, 1989.

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3

Papini, Marcello. Fracture load prediction of structural adhesive joints. Ottawa: National Library of Canada, 1993.

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4

Wanhill, R. J. H. A test plan for sustained load fracture control verification. Amsterdam: National Aerospace Laboratory, 1989.

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5

Martin, Roderick H. Interlaminar fracture characterization: A current review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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6

Rösler, Joachim. Mechanical behaviour of engineering materials: Metals, ceramics, polymers, and composites. Berlin: Springer, 2007.

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7

Minnetyan, Levon. Progression of damage and fracture in composites under dynamic loading. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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8

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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9

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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10

Salem, J. A. Fracture toughness of Si₃N₄ measurement with short bar chevron-notched specimens. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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11

Li, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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12

Carden, Huey D. Unique failure behavior of metal/composite aircraft structural components under crash type loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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13

Kiencke, U. Automotive control systems. Berlin: Springer, 2000.

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14

Ravinder, Chona, Corwin W. R, ASTM Committee E-24 on Fracture Testing., and Symposium on Rapid Load Fracture Testing (1990 : San Francisco, Calif.), eds. Rapid load fracture testing. Philadelphia, PA: ASTM, 1992.

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15

Fernlund, Göran Harald. Analysis and fracture load predictions of structural adhesive joints. 1994.

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16

Wilkowski, G. M. Advances in Fracture and Fatigue for the 1990's: Load History Effects of Fracture Resistance (Pvp, Vol 166). Amer Society of Mechanical, 1989.

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17

J. Singh, Parminder, and Rohit Kotnis. Injury and repair. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.0004.

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♦ Types of injury—traumatic and overuse♦ Importance of determining the energy involved in an injury♦ The relevance of mechanical load curves♦ Types of fracture healing—how and why they occur♦ Healing in articular cartilage, tendon, ligaments, peripheral nerves, and brain tissues.
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18

Behavior of surface and corner cracks subjected to tensile and bending loads in Ti-6A1-4V alloy. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1990.

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19

McNally, Martin A., and Maurizio A. Catagni. Principles of circular external fixation in trauma. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.012015.

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♦ The ideal frame should be versatile, stable during load bearing and allow joint movement, correction of deformity and closed application♦ Circular fixators consist of rings, connecting rods, fine wires and special parts♦ Meticulous preoperative planning with the patient and radiographs is essential♦ Recovery of limb function is the primary goal of fracture care; the patient must be fully involved in the rehabilitation♦ Fixator removal once union is complete should be performed under general anaesthetic for children or with sedation and analgesia in adults
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20

Henry, M. Stress fractures. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199550647.003.012017.

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♦ Stress fractures are fractures occurring as the result of repetitive, submaximal loads, in the absence of a specific precipitating traumatic event.♦ These fractures can be subdivided into two groups on the basis of aetiology. Whereas ‘fatigue fractures’ result from the excessive repetitive (i.e. abnormal) loading of normal bone, ‘insufficiency fractures’ are fractures resulting from normal forces acting on abnormal bone.♦ Early diagnosis allows the initiation of effective treatment that can prevent prolonged pain and disability, as well as avoiding the progression to displacement or a non-union.♦ While management decisions are generally focused on activity modification, protection of weight bearing, and immobilization, there is a subset of fractures at high risk for progression to complete fracture, non-union, or delayed union. These high-risk stress fractures, including tension-side femoral neck fractures and anterior tibial cortex fractures, require aggressive treatment to prevent the sequelae of poor healing.
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21

Center, Langley Research, ed. Test methods for textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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22

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Fracture toughness and crack growth of Zerodur. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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23

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.

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24

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.

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25

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.

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26

O, Harris David, Thomas Jerrell M, George C. Marshall Space Flight Center., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. A review of fracture mechanics life technology. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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27

Tom, Cordes, Lease Kevin, and Society of Automotive Engineers. Fatigue Design and Evaluation Committee., eds. Multiaxial fatigue of an induction hardened shaft. Warrendale, Pennsylvania: SAE, 1999.

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28

Society of Automotive Engineers Fatigue Design and Evaluation committe (Corporate Author), Tom Cordes (Editor), and Kevin Lease (Editor), eds. Multiaxial Fatigue of an Induction Hardened Shaft: Ae-28 (Ae (Series)). Society of Automotive Engineers Inc, 1999.

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29

C, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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30

C, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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31

Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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32

1951-, Scott P., Wilkowski G. M, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., and Battelle Memorial Institute, eds. The effect of cyclic and dynamic loads on carbon steel pipe. Washington, DC: Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1996.

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33

Mechanical Behaviour of Engineering Materials: Metals, Ceramics, Polymers, and Composites. Springer, 2007.

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34

Progression of damage and fracture in composites under dynamic loading. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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35

Fracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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36

Center, Langley Research, ed. Fracture analysis of stiffened panels under biaxial loading with widespread cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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37

H, Hemann John, Gyekenyesi John P, and United States. National Aeronautics and Space Administration., eds. A review of failure models for unidirectional ceramic matrix composites under monotonic loads. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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38

Hughes, Jim. Distal femur and knee. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780198813170.003.0014.

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The knee is one of the main load-bearing joints of the body, and injuries to it can involve damage to the joint or articular surfaces, or fractures to the long bones in case of high-energy trauma. The position of the contralateral leg can cause difficulty in positioning for imaging, but good positioning and technique should allow demonstration of the region for intervention. This chapter covers a selection of orthopaedic procedures involving the distal femur and knee, covering distal femoral plating and LISS plates, tension band wiring of the patella, and cerclage wiring of the patella. Each procedure includes images that demonstrate the position of the C-arm, patient, and surgical equipment, with accompanying radiographs demonstrating the resulting images.
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39

R, Mohan, Battelle Memorial Institute, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., eds. Effects of toughness anisotropy and combined tension, torsion, and bending loads on fracture behavior of ferritic nuclear pipe. Washington, DC: U.S. Nuclear Regulatory Commission, 1995.

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40

A progressive damage methodology for residual strength predictions of notched composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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41

C, Newman J., and Langley Research Center, eds. Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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42

Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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43

P, Phillips E., Everett R. A, and Langley Research Center, eds. Fatigue analyses under constant- and variable-amplitude loading using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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44

Kaufman, J. Gilbert, and Elwin L. Rooy. Aluminum Alloy Castings. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.aacppa.9781627083355.

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Aluminum Alloy Castings: Properties, Processes and Applications is a practical guide to the process, structure, property relationships associated with aluminum alloy castings and casting processes. It covers a wide range of casting methods, including variations of sand casting, permanent mold casting, and pressure die casting, showing how key process variables affect the microstructure, properties, and performance of cast aluminum parts. Other chapters provide similar information on the effects of alloying and heat treating and the influence and control of porosity and inclusions. A significant portion of the book contains curated collections of property and performance data, including many previously unpublished aging response curves, growth curves, and fatigue curves; tensile properties at high and low temperatures and at room temperature after high-temperature exposure; the results of creep rupture tests conducted at temperatures from 212 to 600 °F (100 to 315 °C); and stress-strain curves obtained from casting alloys in various tempers under tensile or compressive loads. The book also discusses the factors that contribute to corrosion and fracture resistance and includes test specimen drawings as well as a glossary of terms. For information on the print version, ISBN 978-0-87170-803-8, follow this link.
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45

J, Minguet Pierre, O'Brien T. Kevin, and Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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46

A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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47

Center, Langley Research, ed. A progressive damage methodology for residual strength predictions of center-crack tension composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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48

Automotive Control Systems: For Engine, Driveline and Vehicle. Society of Automotive Engineers, 2000.

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49

Socie, Darrell, and Gary B. Marquis. Multiaxial Fatigue. SAE International, 1999.

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50

L, Bradley Walter, Texas A & M University. Mechanics and Materials Center., and United States. National Aeronautics and Space Administration., eds. Micromechanics of compression failures in open hole composite laminates: A report. College Station, Tex: Mechanics and Materials Center, Texas A&M University, 1987.

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