Virtual testing and its application in aerospace structural parts

Virtual Testing and Predictive Modeling: For Fatigue and Fracture Mechanics Allowables

Volumn , Issue , 2009, Pages 1-28

  Farahmand, Bahram ^a  

^a Taylor Aerospace (TASS Americas) Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84892210834     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1007/978-0-387-95924-5_1     Document Type: Chapter

References (15)

1. B. Farahmand, Fatigue & Fracture Mechanics of High Risk Parts, Chapman & Hall, 1997, Chapter 5
2. B. Farahmand, Fracture Mechanics of Metals, Composites, Welds, and Bolted Joints, Kluwer Academic Publisher, November 2000, Chapter 6
3. B. Farahmand, "Predicting Fracture and Fatigue Crack Growth Properties Using Tensile Properties, Engineering", J. Fract., Vol. 75, 2007, pp. 2144-2155
4. B. Farahmand, De Xie, F. Abdi, "Estimation of Fatigue and Fracture Allowables for Metallic Materials Under Cyclic Loading", AIAA-2007
5. B. Farahmand, "Multiscaling of Fatigue" Application of virtual testing for obtaining fracture allowables of aerospace and aircraft materials. Springer, 2008 (A Book Chapter by G. Sih)
6. G. Irwin, "Fracture Dynamics", Fracture of Metals, ASM, 1948, p. 147
7. E. Orowan, "Fracture and Strength of Solids", Rep. Prog. Phys., Vol. 12, 1949, pp. 185-232
8. Fatigue Crack Growth Computer Program "NASGRO 4.0", JSC, SRI, ESA, and FAA, 2002
9. MIL-HDBK-5H "Military Handbook Metallic Materials and Elements for Aerospace Vehicle Structure"
10. B. Farahmand, "Virtual Testing for Estimating Material Fracture Properties (Reducing Time & Cost of Testing)", 11th International Conference on Fracture (ICF11), Turin Italy, March 2005
11. NHB 8071 "Fracture Control Requirements for Payloads Using the National Space Transportation System (NSTS)", NASA, Washington, DC, 1985
12. Metal lined Composite Overwrapped Pressure Vessels (COPVs), Arde Inc., 875 Washington Avenue, Carlstadt, New Jersey 07072
13. Military Standard 1522A, "Standard General Requirements for Safe Design Operation of Pressurized Missile and Space System", USA, May 1984
14. B. Farahmand and M. Doyle, "Obtaining Fracture Properties by Virtual Testing and Multiscale Modeling", The Aging Aircraft Conference, 2009
15. B. Farahmand and G. Odegard, "Obtaining Fracture Properties by Virtual Testing and Molecular Dynamics Techniques", The NSTI Conference, 2009