Show simple item record

dc.date.accessioned2017-09-09T17:17:28Z
dc.date.available2017-09-09T17:17:28Z
dc.date.created1928-11-24en_US
dc.identifier.urihttp://hdl.handle.net/11200/48951
dc.descriptionA large number of the metal propellers designed at the Materiel Division have been made from a uniform plan form as to width and thickness and have been variable only as to diameter and initial or designed pitch ratio. A series of model propellers 30 inches in diameter were designed from this plan form, five propellers comprising the series. The five propellers were laid out as true screws for ratios of forward to peripheral velocities of 0.1, 0.2, 0.3, 0.4, and 0.5, respectively. Each propeller was tested at a series of angular settings measured at the 12-inch radius which corresponds to 0.8 times the tip radius. This report includes the results of these tests.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 632en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 2943en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectWind tunnel testingen_US
dc.subjectPropellers, Aerialen_US
dc.subjectAirplanes--Motors--Partsen_US
dc.titleComparison of wind tunnel tests with flight tests on a number of detachable blade propellers made from the same plan form (airplane branch report)en_US
dc.typeTexten_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record