The stability of rotor blade flapping motion

dc.contributor.author	A. G. Shutler	en_US
dc.contributor.author	J. P. Jones	en_US
dc.date.accessioned	2014-10-21T15:54:59Z
dc.date.available	2014-10-21T15:54:59Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/R&M-3178	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3746
dc.description.abstract	An improved method of solving the rotor blade flapping equation is described which avoids the laborious computation of those at present available. Successive approximations to the solution are made but the rapid convergence makes the second approximation sufficient for all practical purposes. The effect of inclining the flapping hinge is considered and an analytical solution including these effects is given in an Appendix. The results show good agreement with an exact solution.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The stability of rotor blade flapping motion	en_US