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V dannoj rabote sproektirowano i smodelirowano krylo samoleta w programme trehmernogo modelirowaniq Catia. V kachestwe materialow dlq kryl'ew samoleta ispol'zuütsq gibridnye kompozitnye Al-splawy i, w chastnosti, uglerodnye i aramidnye wolokna. Dalee byl proweden strukturnyj analiz s pomosch'ü Ansys, w kotorom staticheskij analiz kryla prowodilsq putem prilozheniq dawleniq wozduha dlq dwuh materialow - alüminiq - uglerodnogo wolokna i alüminiq - aramidnogo wolokna. Po rezul'tatam analiza widno, chto deformaciq i naprqzhenie men'she dlq uglerodnogo wolokna, chem dlq aramidnogo. Analiz wibracii takzhe prowoditsq na kryle samoleta dlq dwuh analogichnyh materialow s cel'ü opredeleniq chastot. V ätoj knige w glawe 1 rassmatriwaütsq razlichnye prichiny progressa w proektirowanii i analize aärokosmicheskih detalej i ih materialow. Glawa-2 poswqschena obzoru literatury, glawa-3 - swojstwam i harakteristikam razlichnyh sowremennyh kompozicionnyh materialow i ih primeneniü. V glawe-4 obsuzhdaetsq modelirowanie kompozitnogo kryla samoleta s ispol'zowaniem programmnogo obespecheniq dlq modelirowaniq, takogo kak CATIA, ANSYS. V glawe 5 my obsudili analiz kompozitnogo kryla i ego rezul'taty. Nakonec, my zawershili rabotu zaklüchitel'nymi zamechaniqmi i opisali buduschuü rabotu.