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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2017-11-30T21:45:28Z
dc.date.available2017-11-30T21:45:28Z
dc.date.created1920-09-10en_US
dc.identifier.urihttp://hdl.handle.net/11200/49084
dc.descriptionA model of the VCP-1, modified by reduction of wing area and by improved streamlining of the fuselage, was tested at M.I.T. in June, 1920, in order to determine the proper stabilizer setting and the characteristic lift and lift-drag cures. The characteristic curves are tabulated and plotted.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 107en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1327en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.titleReport on wind tunnel test of Verville racer (airplane section, S. &. A. branch)en_US
dc.typeTexten_US


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