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dc.date.accessioned2017-09-08T20:04:36Z
dc.date.available2017-09-08T20:04:36Z
dc.date.created1928-11-24en_US
dc.identifier.urihttp://hdl.handle.net/11200/48942
dc.descriptionAmong the large number of methods which have been used to predict performance, those found most reliable depend, for a determination of the structural resistance, on comparison with other designs whose performance is known. This report is limited to the presentation of information which will be useful in predicting the maximum level speed, ignoring other performance factors, such as rate of climb and ceiling. The determination of the equivalent flat plate area of an airplane from the maximum level speed involves few assumptions, and comparison of the results obtained from a large number of representative airplanes affords a reliable basis on which to determine the high speed of a new design.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 629en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 2919en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectDrag (Aerodynamics)en_US
dc.subjectMathematics--Formulaeen_US
dc.subjectAerodynamic measurementsen_US
dc.subjectBiplanesen_US
dc.titleDetermination of structural airplane drag (airplane branch report)en_US
dc.typeTexten_US


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