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Impact test of a JN-4 tail skid and landing chassis (airplane section report)


Metadata FieldValueLanguage
dc.creatorWeaver, D. B.en_US
dc.date.accessioned2018-09-18T20:24:09Z
dc.date.available2018-09-18T20:24:09Z
dc.date.created1923-04-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/49291
dc.descriptionThis test was conducted for the purpose of determining the height from which both tail skid and landing chassis could be dropped before failure. The tail skid held satisfactory when dropped from a 30-inch height with a 9 1/2 degree inclination to the vertical. The landing chassis held up satisfactorily for the 48-inch drop with half load, approximately a 24-inch drop with full load.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 5, no. 409en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2018en_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.titleImpact test of a JN-4 tail skid and landing chassis (airplane section report)en_US
dc.typeTexten_US

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