Effect of space limitations on spring performance is analyzed and leads to optimum design formulas for three most common types of aircraft springs, i.e., tension, compression, and torsion springs; using formulas thus derived, for given allowable stress relationship between space limitations, maximum load obtainable and corresponding wire size can be found immediately.
Space limitations and optimum conditions in aircraft spring design
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 10 , n 2 ; p 51-57
1943
7 pages
Article (Journal)
English
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