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dc.date.accessioned2017-09-08T18:53:34Z
dc.date.available2017-09-08T18:53:34Z
dc.date.created1929-09-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48936
dc.descriptionThis report presents the results obtained in the investigation of a particular method of determining under what conditions or combinations of conditions (aerodynamic, dynamic, and elastic) undamped, destructive oscillations are set up in internally braced wings. The method of attach was developed as the first step toward determining the causes and prevention of dynamic instability of wings or "wing flutter," and was considered necessary in view of the fact that no solution so far existed that could be accepted as a basis for establishing the necessary criteria for judging the stability of specific internally braced wings. It was also decided to attempt to build a piece of apparatus in which the important variables could each be adjusted independently of the others or in combination with any or all of the others.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C.: Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 635en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 3002en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectFlutter (Aerodynamics)en_US
dc.subjectAirplanes--Wingsen_US
dc.subjectMathematics--Formulaeen_US
dc.titleStudy of wing flutter. Part I. Test of apparatus and discussion of procedure (airplane branch report)en_US
dc.typeTexten_US


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