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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-07-31T14:06:15Z
dc.date.available2018-07-31T14:06:15Z
dc.date.created1921-04-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/49187
dc.descriptionThe purpose of this investigation is to obtain comprehensive data on the performance of the standard sizes of airplane tires and wheels in the clincher types, and the existing straight side types size, with special reference to the load-deflection curves of the tires and ultimate strength of the various sizes of wheels. From the curves obtained in the foregoing tests, it is possible to determine the size of the wheel, size of tire, and the most satisfactory air pressure to use for any particular airplane when the weight is known. In addition, the factor of safety can be calculated from the information relative to the breaking load of wheels of various sizes.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 270en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1496en_US
dc.subjectWheelsen_US
dc.subjectTiresen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Tiresen_US
dc.subjectAirplanes--Landing gearen_US
dc.titleResults of static tests on standard airplane tires and wheels (material section report)en_US
dc.typeTexten_US


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