This text provides students who have had statics and introductory strength of materials with the necessary tools to perform stress analysis on aerospace structures such as wings, tails, fuselages, and space frames. It progresses from introductory continuum mechanics through strength of materials of thin--walled structures to energy methods, culminating in an introductory chapter on the powerful finite element method.
Audience: Tertiary; University or College
Number Of Pages: 528
Published: 6th February 1985
Publisher: John Wiley and Sons Ltd
Country of Publication: US
Dimensions (cm): 24.25 x 16.85 x 3.11
Edition Number: 1