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Notes on airplane flight endurance (I) (airplane section, S. & A. branch report)


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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-01T20:12:57Z
dc.date.available2018-08-01T20:12:57Z
dc.date.created1921-05-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/49205
dc.descriptionIt is the purpose of this report to describe a chart which will serve as a ready means of determining for any airplane the minimum horsepower required or the maximum horsepower available at any altitude which it is possible for the airplane to reach. The chart should be useful in calculations of airplane-flight endurance for determining (a) the maximum time in the air with a given fuel supply at the altitude of minimum horsepower required; (b) the corresponding speed; (c) the fuel supply necessary for a given duration at any altitude, either at full power or with throttled engines. In addition the curves of horsepower at altitude as presented may be used to indicate absolute ceiling.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 210en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1458en_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Fuel consumptionen_US
dc.subjectHorsepowereng
dc.subjectAirplanes--Fuel systemsen_US
dc.subjectAirplanes--Handling characteristicsen_US
dc.titleNotes on airplane flight endurance (I) (airplane section, S. & A. branch report)en_US
dc.typeTexten_US

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