Exact mathematical treatment of problem is possible by replacing propeller blade by homogeneous prismatic rod; conclusions can then be drawn as to behavior of actual propeller; natural frequencies are determined and stressing of systems under various vibration modes are discussed. Indexed in Engineering Index 1939 p 50, from Deutsche Luftfahrtforschung Jahrbuch 1938 p II-141-59.
Coupling of flexural propeller vibrations with torsional crankshaft vibrations
Nat Advisory Committee Aeronautics -- Tech Memo
1943
46 pages
9 Supp sheets
Report
Englisch
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