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Pressure distribution over the stabilizer of the Vought VE-7 airplane (airplane section report)


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dc.creatorHaskins, G. W.en_US
dc.creatorCarroll, F. O.en_US
dc.date.accessioned2018-09-18T21:16:50Z
dc.date.available2018-09-18T21:16:50Z
dc.date.created1923-04-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/49296
dc.descriptionThe purpose of this investigation was to determine the pressure distribution over the horizontal surfaces of the VE-7 airplane at various altitudes of flight. Readings were obtained only on the right-hand stabilizer. Flight tests were run under the conditions of (a) normal flight, (b) diving to high speeds, (c) pulling out of dive suddenly, and (d) stalling, the last of which was run with engine speeds of 600 revolutions per minute and 1,700 revolutions per minute in order to determine the effect of the slip stream. Practically all tests were run at an altitude of 5,000 feet.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 5, no. 419en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2022en_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectStrains and stressesen_US
dc.subjectAir flowen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectVought aircraften_US
dc.titlePressure distribution over the stabilizer of the Vought VE-7 airplane (airplane section report)en_US
dc.typeTexten_US

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