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dc.creatorLyons, P. M.en_US
dc.date.accessioned2017-07-17T19:43:07Zen_US
dc.date.available2017-07-17T19:43:07Zen_US
dc.date.created1926-09-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/48905
dc.descriptionThis document is a supplement to Air Service Information Circular, Vol. 6, No. 511, Wind tunnel test of six horizontal tail surface designs having the U.S.A.-47 airfoil section (airplane section report). The object of this test was to determine the elevator moments about the hinge line on this balanced tail surface.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of the Air Corpsen_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2675en_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 6, no. 567en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Tail surfacesen_US
dc.subjectElevators (Airplanes)en_US
dc.titleWind tunnel test for elevator hinge moment coefficients on the horizontal tail surface no. 5 with balanced elevator (supplementary to Serial Report 2463, A.S. Information Circular, Vol. 6, No. 511) (airplane section report)en_US
dc.typeTexten_US


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