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Wing flap test of a DH-4B wind tunnel model (airplane section report)


Metadata FieldValueLanguage
dc.creatorLyons, P. M.en_US
dc.date.accessioned2017-06-28T17:13:42Zen_US
dc.date.available2017-06-28T17:13:42Zen_US
dc.date.created1926-01-25en_US
dc.identifier.urihttp://hdl.handle.net/11200/48849
dc.descriptionThe object of this test was to determine the aerodynamic characteristics of this model as affected by adjustable wing flaps. Tests were run on this 1/24 scale model in the McCook Field 5-foot wind tunnel at 20 and 40 miles per hour.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 552en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2587en_US
dc.subjectBiplanesen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAeronautics--Researchen_US
dc.subjectAirplanes--Wingsen_US
dc.titleWing flap test of a DH-4B wind tunnel model (airplane section report)en_US
dc.typeTexten_US

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