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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-07-20T16:36:42Z
dc.date.available2018-07-20T16:36:42Z
dc.date.created1921-07-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49176
dc.descriptionThe object of this test was to determine if the strength of the shock-absorbing wheels substantiates the claims made for them, together with the possibility of using them with the standard Curtiss JA-4 chassis struts with a heavier axle.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 254en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1595en_US
dc.subjectWheelsen_US
dc.subjectStruts (Engineering)en_US
dc.subjectShock absorbersen_US
dc.subjectStrength of materialsen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.titleReport of static test on the J.V. Martin shock-absorbing wheels with the Curtiss JN-4 chassis (airplane section, S. & A. branch)en_US
dc.typeTexten_US


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