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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-10T15:54:36Z
dc.date.available2018-08-10T15:54:36Z
dc.date.created1922-03-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49231
dc.descriptionThe object of the investigation covered by this report was to determine the effect of changes in wing loading and aspect ratio on the performance and weight of single-seater pursuit airplanes. This information was obtained by making six preliminary wing designs for an airplane of this type using two aspect ratios and three wing loadings. The conclusion was that the lighter the wing loading the better will be the performance of a single-seater pursuit airplane in most particulars.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 4, no. 315en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1740en_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectFighter planesen_US
dc.subjectStrains and stresses
dc.titleDetermination of the best wing loading for single-seater pursuit airplanes (airplane section, S. & A. branch)en_US
dc.typeTexten_US


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