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Report of wind tunnel tests on aerofoils: Dayton-Wright nos. TT-1 and TT-2, Dayton-Wright nos. 5 and 6, and Gottingen no. 387 (airplane section, S. & A. branch)


Metadata FieldValueLanguage
dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-13T19:03:26Z
dc.date.available2018-08-13T19:03:26Z
dc.date.created1922-03-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49236
dc.descriptionThe Dayton-Wright nos. TT-1 and TT-2, Dayton-Wright nos. 5 and 6, and Gottingen no. 387 aerofoils were tested at Massachusetts Institute of Technology during June and August, 1921, to determine lift, drag, L/D, center of pressure, and moments about the leading edge.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 4, no. 328en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1769en_US
dc.subjectAerofoilsen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAerodynamic measurementsen_US
dc.titleReport of wind tunnel tests on aerofoils: Dayton-Wright nos. TT-1 and TT-2, Dayton-Wright nos. 5 and 6, and Gottingen no. 387 (airplane section, S. & A. branch)en_US
dc.typeTexten_US

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