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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2017-12-12T20:54:49Z
dc.date.available2017-12-12T20:54:49Z
dc.date.created1920-12-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/49111
dc.descriptionThis document describes testing of the D. H.-4 airplane equipped with the 300 H.P. Hispano-Squiza engine, with the X-19925 propeller. The flight testing was performed without full military load. Measurements include speed and climb rate.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 155en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1371en_US
dc.subjectPropellers, Aerialen_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes, Militaryen_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Motorsen_US
dc.subjectDe Havilland aircraften_US
dc.titlePerformance test of D. H.-4 with 200 h. p. Hispano-Suiza engine showing performance with propeller X-19925. Flight test branch. (performance test report no. 49)en_US
dc.typeTexten_US


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