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dc.creatorMorse, Alan L.en_US
dc.date.accessioned2017-06-22T18:47:15Z
dc.date.available2017-06-22T18:47:15Z
dc.date.created1925-09-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48832
dc.descriptionThe object of this test was to determine the aerodynamic characteristics of a model using the above design with the two sets of control surfaces. The report includes graphs of test results, diagrams of the model design, and photographs showing the model from 4 different angles.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 531en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2469en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.subjectBiplanesen_US
dc.subjectBombersen_US
dc.titleWind tunnel test of a heavy bomber study 1/40 scale model with large and small control surfaces (airplane section report)en_US
dc.typeTexten_US


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