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Aircraft Structure I

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Course Description

​Principles of stressed skin construction: materials and structural components of aircraft,Airworthiness and Airframe Loads,Bending, shear and torsion of open and closed thin-walled beams, Structural idealization,Stress analysis of aircraft components: wing spars and box beams, fuselages, wings, fuselage frames and wing ribs and laminated composite structures.​

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Course Syllabus
Created at 11/21/2017 15:03 by YAZAN TAAMNEH
Last modified at 10/30/2020 1:48 by ABDALLAH ALMOMANI