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Study of wing flutter. Part II. Continuation of tests on revised apparatus at Wright Field wind tunnel (Supplement to Part I--Test of apparatus and discussion of procedure A.D.M. 1014, dated October 20, 1928) (airplane branch report)


Metadata FieldValueLanguage
dc.creatorGreene, Carl F.en_US
dc.creatorYounger, John E.en_US
dc.date.accessioned2016-05-25T18:51:14Z
dc.date.available2016-05-25T18:51:14Z
dc.date.created1930-08-30en_US
dc.date.issued1930-08-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/48596
dc.descriptionThis investigation is a continuation of a series of experiments initiated by the authors for determining the influence of the physical characteristics of an airfoil on its tendency to flutter in an air stream. In this series of experiments, the following characteristics were investigated: 1. The extent to which the aileron participates in the action of flutter. 2. The effect of variation of the natural torsional period of the wing. 3. The effect of the camber of an airfoil on the critical velocity at which flutter is precipitated. 4. The effect of the location of the elastic axis. 5. The effect of the distribution of the mass of the airfoil. 6. The effect of the size of the airfoil.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C.: Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 653en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 3237en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectFlutter (Aerodynamics)en_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Wingsen_US
dc.titleStudy of wing flutter. Part II. Continuation of tests on revised apparatus at Wright Field wind tunnel (Supplement to Part I--Test of apparatus and discussion of procedure A.D.M. 1014, dated October 20, 1928) (airplane branch report)en_US
dc.typeTexten_US
dc.relation.referencesStudy of Wing Flutter. Part I. Test of apparatus and discussion of procedure A.D.M. 1014en_US

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