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…mehr
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.
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.
Inhaltsangabe
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.
