Hybrid Anisotropic Materials for Structural Aviation Parts
Autor Yosif Golfmanen Limba Engleză Hardback – 5 noi 2010
Tools to ensure cost-effective, optimized fabrication of aircraft, satellites, space vehicles, and more…
With a focus on analytic modeling and dynamic analysis of anisotropic hybrid materials used in structural parts, this book assesses how and why design mechanisms either work or fail. It describes how current manufacturing techniques can apply alternative electronic and ultrasonic systems to improve the strength of an aircraft’s parts, reduce vibrations, and counteract deicing effects, among other vital requirements.
Presenting valuable case studies involving manufacturers such as Boeing and DuPont, this book covers topics including:
- Nano composites, impregnation processes, and stress/strain analysis
- New techniques for analyzing interlaminar shear distribution sandwich/carbon/fiber/epoxy technologies
- Non-destructive methods, control technological parameters, and the influence of technological defects
- Use of carbon–silicon nanotubes and ceramic technology
- Strength criteria and analysis, and composite life prediction methodologies
- Dynamic aspects and stability of jetliners and lattice aviation structures
- Interlaminar shear stress analysis and possible failure
- Fatigue strength and vibration analysis
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Specificații
ISBN-13: 9781439836804
ISBN-10: 1439836809
Pagini: 340
Ilustrații: 523 Equations; 76 Tables, black and white; 113 Illustrations, black and white
Dimensiuni: 156 x 234 x 23 mm
Greutate: 0.61 kg
Ediția:1
Editura: CRC Press
Colecția CRC Press
ISBN-10: 1439836809
Pagini: 340
Ilustrații: 523 Equations; 76 Tables, black and white; 113 Illustrations, black and white
Dimensiuni: 156 x 234 x 23 mm
Greutate: 0.61 kg
Ediția:1
Editura: CRC Press
Colecția CRC Press
Public țintă
Aerospace and aeronautical design engineers and researchers, materials scientists, as well as grad students in engineering and materials science.Cuprins
Nanocomposite Automation Process. Impregnation Process. Strength Criteria and Dynamic Stability. Interlaminar Shear Stress Analysis. Fatigue Strength, Stress, and Vibration Analysis. NDE Methods Control Properties. Coating Process Protective Aviation Parts.
Notă biografică
Involved in R&D composites since 1960, Yosif Golfman graduated from the Shipbuilding Technology Institute, Leningrad, USSR, and received his Ph.D. in 1969, working as a research composite engineer there afterward. He has worked investigating the influence of technological factors on the strength of fiberglass propellers and blades. In the United States, he worked as a research engineer at Ad Tech Systems Research in Dayton, Ohio, as a mechanical engineer at Foster-Miller, Inc., Waltham, Massachusetts, and as a process mechanical engineer at Spectran, Inc., in Sturbridge, Massachusetts. At Neo-Advent Technologies, Inc., Littleton, Massachusetts, he worked on design, technology development, and manufacturing of lightweight nanoscale structures parts, based on ceramic, and thermoplastic, and liquid polymers, and carbon fiber textiles for aerospace applications and avionics.
Recenzii
As one might expect the mathematical content is extensive and of a highly specialized nature, but not to the extent that those lacking mathematical skills should be discouraged. … The author rightly claims credit for his early pioneering work on ultrasonic waves and is well qualified to advance the use of ultrasonic testing. … the technical content of the book supported by over 300 cutting-edge references is admirable and cannot be faulted.
—Peter C. Gasson, The Aeronautical Journal, March 2012
—Peter C. Gasson, The Aeronautical Journal, March 2012
Descriere
As a professional in the field of composite research for 40 years, Yosif Golfman wrote this text to provide unique information on the use of anistropic materials in aerospace design. It covers nano composites, impregnation processes, and stress/strain analysis in aerospace structural engineering. It features new methods for analysis of interlaminar shear distribution in sandwich/carbon/fiber/epoxy technologies. It also discusses non-destructive methods, control technological parameters, and the influence of technological defects, such as micro-cracks, on the reduction of fatigue strength and durability. It also considers the protection of composite helicopter rotor blades by polymer coating layers.