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dc.creatorFriel, E. C.en_US
dc.date.accessioned2017-09-09T18:28:08Z
dc.date.available2017-09-09T18:28:08Z
dc.date.created1928-08-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48956
dc.descriptionThe increased trend in airplane design toward metal construction has focused the attention of airplane designers upon many new problems. Chief among these problems is that of metal-wing construction and, in particular, metal-spar design. In general, the methods used in wood-spar design are adaptable to the constant depth, continuous web metal spar. With respect to trussed metal spars, however, the methods of design have been quite arbitrary. This report may be considered to be roughly divided into three parts, namely: (1) Discussion and outline of preliminary design; (2) Theory, development, and outline of precise design or analysis; and (3) Illustrative examples and proof of precise methods.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 621en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 2880en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectMathematics--Formulaeen_US
dc.titleDesign of trussed metal spars for single bay airplanes (airplane branch report)en_US
dc.typeTexten_US


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