Tables for computing the instantaneous velocities induced at the blade axes of a lifting rotor in forward flight by the skewed helical wake vortices and a method for calculating the resultant blade air : a theoretical analysis

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dc.contributor.author Castles, Walter en_US
dc.contributor.author Durham, Howard L. en_US
dc.date.accessioned 2012-01-19T12:30:53Z
dc.date.available 2012-01-19T12:30:53Z
dc.date.issued 1959 en_US
dc.identifier.other 327299 en_US
dc.identifier.uri http://hdl.handle.net/1853/42244
dc.description Issued as ASTIA Doc. no. AD-210 613 and [Final report] Project no. A-365 en_US
dc.description Contract no. Nonr 991(05) en_US
dc.publisher Georgia Institute of Technology en_US
dc.relation.ispartofseries Engineering Experiment Station ; Project no. A-365 en_US
dc.subject.lcsh Rotors (Helicopters) Aerodynamics en_US
dc.title Tables for computing the instantaneous velocities induced at the blade axes of a lifting rotor in forward flight by the skewed helical wake vortices and a method for calculating the resultant blade air : a theoretical analysis en_US
dc.type Technical Report en_US
dc.contributor.corporatename Georgia Institute of Technology. Office of Sponsored Programs en_US
dc.contributor.corporatename Georgia Institute of Technology. Engineering Experiment Station en_US


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