Design of composite helicopter rotor blades to meet given cross sectional stiffness properties
Design of composite helicopter rotor blades to meet given cross sectional stiffness properties
| dc.contributor.author | Lemanski, S.L. | |
| dc.contributor.author | Weaver, P.M. | |
| dc.contributor.author | Hill, G.F.J. | |
| dc.date.accessioned | 2016-06-29T16:51:13Z | |
| dc.date.available | 2016-06-29T16:51:13Z | |
| dc.date.issued | 2002 | |
| dc.identifier.other | ERF200273 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/451 | |
| dc.language.iso | en | |
| dc.subject.other | Structures and Materials | |
| dc.title | Design of composite helicopter rotor blades to meet given cross sectional stiffness properties |
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