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Static test of the Curtiss XO-1 observation airplane (airplane section report)

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dc.creatorWeaver, D. B.en_US
dc.descriptionThis static test was conducted for the purpose of determining the structural strength of the Curtiss XO-1 airplane submitted during the contest for corp-observation airplanes, December 1924, and purchased on contract No. 727. Tests included: wing cellule tests; leading edge static tests; ailerons tests; stabilizer and elevator tests; rudder and fin tests; landing chassis tests; fuel tank release mechanism tests; fuselage tests; tail skid impact tests. Results of the tests are reported, along with design recommendations based on those results.en_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 539en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2523en_US
dc.subjectCurtiss aircraften_US
dc.subjectAirplanes, Militaryen_US
dc.subjectElevators (Airplanes)en_US
dc.subjectAirplanes--Fuel systemsen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAirplanes--Control surfacesen_US
dc.subjectAirplanes--Design and constructionen_US
dc.titleStatic test of the Curtiss XO-1 observation airplane (airplane section report)en_US

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