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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2017-12-15T19:10:19Z
dc.date.available2017-12-15T19:10:19Z
dc.date.created1921-01-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49120
dc.descriptionThis document describes investigation of stresses in cabane struts under three conditions of loading: high incidence, low incidence, and reversed flight.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 172en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1376en_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Shock absorbersen_US
dc.subjectStruts (Engineering)en_US
dc.subjectStrains and stressesen_US
dc.subjectShock absorbersen_US
dc.titleStructural design of cabane struts for the PW-1 with R. A. F. 15 taped wings (airplane section, S. & A. branch)en_US
dc.typeTexten_US


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