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dc.creatorMiddleton, R. E.en_US
dc.creatorDePort, Theoen_US
dc.date.accessioned2017-09-21T19:54:01Z
dc.date.available2017-09-21T19:54:01Z
dc.date.created1932-06-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/48993
dc.descriptionThe purpose of this test was to determine the shock-absorption capacity of the strut, and to make a comparison between it and the Gruss stut, model C-68-1, which is used on the Fokker Y1C-14 airplane. The test shows that the Gruss model X-58 has performance characteristics much superior to model C-68-1, and that it is better suited for use on the Fokker Y1C-14 airplane.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 671en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 3499en_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Shock absorbersen_US
dc.subjectStruts (Engineering)en_US
dc.subjectFokker airplanesen_US
dc.subjectShock absorbersen_US
dc.titleDynamic test of Gruss shock absorber model X-58 (airplane branch report)en_US
dc.typeTexten_US


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