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

Metadata Field	Value	Language
dc.creator	Haskins, G. W.	en_US
dc.creator	Carroll, F. O.	en_US
dc.date.accessioned	2018-09-18T21:16:50Z
dc.date.available	2018-09-18T21:16:50Z
dc.date.created	1923-04-01	en_US
dc.identifier.uri	http://hdl.handle.net/11200/49296
dc.description	The 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.format	PDF	en_US
dc.publisher	Washington, D.C. : Chief of Air Service	en_US
dc.relation.ispartofseries	Air Service information circular (Aviation) ; v. 5, no. 419	en_US
dc.relation.ispartofseries	McCook Field report ; Serial no. 2022	en_US
dc.subject	Aeronautics--Systems engineering	en_US
dc.subject	Airplanes--Design and construction	en_US
dc.subject	Strains and stresses	en_US
dc.subject	Air flow	en_US
dc.subject	Airplanes--Flight testing	en_US
dc.subject	Airplanes--Parts--Testing	en_US
dc.subject	Vought aircraft	en_US
dc.title	Pressure distribution over the stabilizer of the Vought VE-7 airplane (airplane section report)	en_US
dc.type	Text	en_US

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