Derek G Spear (USA Air Force Institute of Technology), Anthony N Palazotto (USA Air Force Institute of Technology)
Testing and Modeling of Cellular Materials
Derek G Spear (USA Air Force Institute of Technology), Anthony N Palazotto (USA Air Force Institute of Technology)
Testing and Modeling of Cellular Materials
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Testing and Modeling of Cellular Materials discusses the characterization of cellular lattices through quasi-static and dynamic testing for use in light-weighting or energy absorbing applications.
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Testing and Modeling of Cellular Materials discusses the characterization of cellular lattices through quasi-static and dynamic testing for use in light-weighting or energy absorbing applications.
Produktdetails
- Produktdetails
- Verlag: Taylor & Francis Ltd
- Seitenzahl: 184
- Erscheinungstermin: 19. Dezember 2024
- Englisch
- Abmessung: 156mm x 233mm x 15mm
- Gewicht: 322g
- ISBN-13: 9781032290249
- ISBN-10: 1032290242
- Artikelnr.: 72110687
- Herstellerkennzeichnung
- Libri GmbH
- Europaallee 1
- 36244 Bad Hersfeld
- gpsr@libri.de
- Verlag: Taylor & Francis Ltd
- Seitenzahl: 184
- Erscheinungstermin: 19. Dezember 2024
- Englisch
- Abmessung: 156mm x 233mm x 15mm
- Gewicht: 322g
- ISBN-13: 9781032290249
- ISBN-10: 1032290242
- Artikelnr.: 72110687
- Herstellerkennzeichnung
- Libri GmbH
- Europaallee 1
- 36244 Bad Hersfeld
- gpsr@libri.de
Dr. Derek G. Spear completed his MS in Aerospace Engineering at the North Carolina State University in Raleigh, NC, and his MS in Aviation Systems at the University of Tennessee in Knoxville, TN. He obtained his PhD in Aeronautical Engineering from the Air Force Institute of Technology, Wright-Patterson Air Force Base, OH. He has assumed various roles as executive officer/instructor pilot, flight commander/program manager, test pilot, helicopter flight commander, flight safety officer, director of operations, and commander. He has received many awards, honors, and decorations for his services. He has published white papers and presented his research work at international conferences. Dr. Anthony N. Palazotto is a Distinguished Professor, Aerospace Engineering at the Air Force Institute of Technology. He has over 50 years of experience in administration, research, and education within an Engineering College. He supervised and administered faculty within a departmental division. He developed research efforts and course offerings in composite materials, wave mechanics, elasticity, shells, fracture mechanics, and finite element techniques. He is highly involved in technical society activity as chairperson and founder of various committees. He was the author of over 700 presentations and publications, 271 are archival.
1. Introduction. 2. Background Theory. 3. Experimental Methodology. 4.
Uniaxial Compression of Lattices. 5. Mechanical Properties of Lattices and
Design Variations. 6. Split Hopkinson Pressure Bar Test Results. 7. Strain
Rate-Sensitive Constitutive Model for Lattice Structure. 8. Lattice Damage
Model. 9. Computational Modeling Techniques and Results. 10. Projectile
Impact Results. 11. Conclusions.
Uniaxial Compression of Lattices. 5. Mechanical Properties of Lattices and
Design Variations. 6. Split Hopkinson Pressure Bar Test Results. 7. Strain
Rate-Sensitive Constitutive Model for Lattice Structure. 8. Lattice Damage
Model. 9. Computational Modeling Techniques and Results. 10. Projectile
Impact Results. 11. Conclusions.
1. Introduction. 2. Background Theory. 3. Experimental Methodology. 4.
Uniaxial Compression of Lattices. 5. Mechanical Properties of Lattices and
Design Variations. 6. Split Hopkinson Pressure Bar Test Results. 7. Strain
Rate-Sensitive Constitutive Model for Lattice Structure. 8. Lattice Damage
Model. 9. Computational Modeling Techniques and Results. 10. Projectile
Impact Results. 11. Conclusions.
Uniaxial Compression of Lattices. 5. Mechanical Properties of Lattices and
Design Variations. 6. Split Hopkinson Pressure Bar Test Results. 7. Strain
Rate-Sensitive Constitutive Model for Lattice Structure. 8. Lattice Damage
Model. 9. Computational Modeling Techniques and Results. 10. Projectile
Impact Results. 11. Conclusions.