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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-01T18:57:01Z
dc.date.available2018-08-01T18:57:01Z
dc.date.created1921-04-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/49197
dc.descriptionThis test was made to determine the effect of static loading on a 36 by 8 inch airplane wheel and tire, which was built in accordance with the tentative rim standards of the Tire and Rim Association. The action of the wheel under static loading is satisfactory. This wheel is suitable for the Handley-Page airplane.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 207en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1435en_US
dc.subjectWheelsen_US
dc.subjectTiresen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Tiresen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.titleReport on 36 x 8 inch straight-side tire and wheel (material section report no. 114)en_US
dc.typeTexten_US


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