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dc.creatorNewell, J. S.en_US
dc.date.accessioned2018-09-11T19:30:11Z
dc.date.available2018-09-11T19:30:11Z
dc.date.created1923-02-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49281
dc.descriptionWith the development of large internally braced airplane wings, the simple two-spar type of construction appears to be uneconomical as regards material and weight. Accordingly three or more spars are sometimes employed, and with the introduction of this multispar construction comes the question as to the manner in which the load on the wing is distributed among the spars. The following report covers an investigation of a number of methods of apportioning the load as applied to a large three-spar metal wing; a study of the results obtained as compared with the distribution indicated by the sand test of this wing, and the conclusions based upon that study.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 4, no. 394en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2005en_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectAerodynamic loaden_US
dc.subjectStrains and stressesen_US
dc.titleDistribution of load among the spars in multi-spar construction of airplane wings (airplane section report)en_US
dc.typeTexten_US


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