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100   $a20180331d2011      uy             0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aHybrid anisotropic materials for structural aviation parts /$fYosif Golfman
210  1$aBoca Raton :$cCRC Press,$d2011.
215   $a1 online resource (338 p.)
300   $aDescription based upon print version of record.
311   $a1-322-61600-0 
311   $a1-4398-3680-9 
320   $aIncludes bibliographical references and index.
327   $aFront 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 cover
330   $aOptimization 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 of
606   $aAirframes$xMaterials
606   $aComposite materials
606   $aAnisotropy
615  0$aAirframes$xMaterials.
615  0$aComposite materials.
615  0$aAnisotropy.
676   $a629.134/3
700   $aGolfman$b Yosif.$0478160
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910785316203321
996   $aHybrid anisotropic materials for structural aviation parts$9265162
997   $aUNINA