02701oam 2200613I 450 991078531620332120230725025707.00-429-10620-31-62870-934-01-4398-3681-710.1201/b10294 (CKB)2670000000059441(EBL)624981(OCoLC)693771891(SSID)ssj0000420121(PQKBManifestationID)11929578(PQKBTitleCode)TC0000420121(PQKBWorkID)10385581(PQKB)10660730(MiAaPQ)EBC624981(Au-PeEL)EBL624981(CaPaEBR)ebr10437672(CaONFJC)MIL692882(EXLCZ)99267000000005944120180331d2011 uy 0engur|n|---|||||txtccrHybrid anisotropic materials for structural aviation parts /Yosif GolfmanBoca Raton :CRC Press,2011.1 online resource (338 p.)Description based upon print version of record.1-322-61600-0 1-4398-3680-9 Includes bibliographical references and index.Front cover; Contents; Preface; Acknowledgments; Chapter 1. Nanocomposite Automation Process; Chapter 2. Impregnation Process; Chapter 3. Strength Criteria and Dynamic Stability; Chapter 4. Interlaminar Shear Stress Analysis; Chapter 5. Fatigue Strength, Stress, and Vibration Analysis; Chapter 6. NDE Methods Control Properties; Chapter 7. Protective Coating Process for Aviation Parts; Back coverOptimization 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 application examples to help the reader establish a solid understanding of anisotropic properties, theory of laminates, and basic fabrication technologies. Tools to ensure cost-effective, optimized fabrication ofAirframesMaterialsComposite materialsAnisotropyAirframesMaterials.Composite materials.Anisotropy.629.134/3Golfman Yosif.478160MiAaPQMiAaPQMiAaPQBOOK9910785316203321Hybrid anisotropic materials for structural aviation parts265162UNINA