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Wind tunnel test of 1/24 scale model of the Douglas O-2E-1 airplane wing cellule through 360 degrees (airplane branch)


Metadata FieldValueLanguage
dc.creatorBorden, D. M.en_US
dc.date.accessioned2017-09-09T17:32:35Z
dc.date.available2017-09-09T17:32:35Z
dc.date.created1928-02-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48953
dc.descriptionThe object of this test was to determine the general aerodynamic characteristics of a 1/24-scale model of the Douglas O-2E-1 airplane wing cellule through 360 degrees.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 612en_US
dc.relation.ispartofseriesMateriel Division report ; Serial no. 2832en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.titleWind tunnel test of 1/24 scale model of the Douglas O-2E-1 airplane wing cellule through 360 degrees (airplane branch)en_US
dc.typeTexten_US

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