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Report on wind-tunnel test of armored pursuit airplane PG-1, type IV (airplane section, S. & A. branch)


Metadata FieldValueLanguage
dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2017-12-15T19:48:12Z
dc.date.available2017-12-15T19:48:12Z
dc.date.created1921-05-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/49124
dc.descriptionA model of an armored single-seater pursuit airplane for ground work, designed by Engineering Division, was tested at M. I. T., December 1920. The usual tests for forces and moments with various settings of the tail plane were made. The data is given in the accompanying tables and figures.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 166en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1499en_US
dc.subjectWind tunnel testingen_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.subjectAirplanes, Militaryen_US
dc.titleReport on wind-tunnel test of armored pursuit airplane PG-1, type IV (airplane section, S. & A. branch)en_US
dc.typeTexten_US

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