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dc.contributor.authorCastles, Walteren_US
dc.contributor.authorDurham, Howard L.en_US
dc.date.accessioned2012-01-19T12:30:53Z
dc.date.available2012-01-19T12:30:53Z
dc.date.issued1959en_US
dc.identifier.other327299en_US
dc.identifier.urihttp://hdl.handle.net/1853/42244
dc.descriptionIssued as ASTIA Doc. no. AD-210 613 and [Final report] Project no. A-365en_US
dc.descriptionContract no. Nonr 991(05)en_US
dc.publisherGeorgia Institute of Technologyen_US
dc.relation.ispartofseriesEngineering Experiment Station ; Project no. A-365en_US
dc.subject.lcshRotors (Helicopters) Aerodynamicsen_US
dc.titleTables 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 analysisen_US
dc.typeTechnical Reporten_US
dc.contributor.corporatenameGeorgia Institute of Technology. Office of Sponsored Programsen_US
dc.contributor.corporatenameGeorgia Institute of Technology. Engineering Experiment Stationen_US
dc.contributor.corporatenameGeorgia Institute of Technology. Office of Sponsored Programs


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