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

chapter 1|62 pages

Nanocomposite Automation Process

chapter 2|22 pages

Impregnation Process

chapter 3|76 pages

Strength Criteria and Dynamic Stability

chapter 4|38 pages

Interlaminar Shear Stress Analysis

chapter 6|50 pages

NDE Methods Control Properties