Optimization of aviation and space vehicle design requires accurate assessment of the dynamic stability and general properties of hybrid materials used in aviation parts. Written by a professional with 40 years of experience in the field of composite research, Hybrid Anisotropic Materials for Structural Aviation Parts provides key analysis and appl
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.