Publikationsdatum:
2019-07-11
Beschreibung:
The exact mathematical treatment of the problem is possible by replacing the propeller blade by a homogeneous prismatic rod. Conclusions can them be drawn as to the behavior of an actual propeller, since tests on propeller blades have indicated a qualitative agreement with the homogeneous rod. The natural frequencies are determined and the stressing of the systems under the various vibration modes are discussed.
Schlagwort(e):
Mechanical Engineering
Materialart:
NACA-TM-1051
,
Jahrbuch 1938 der Deutschen Luftfahrtforschung; 141-159
Format:
application/pdf
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