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 Field | Value | Language |
|---|---|---|
| dc.creator | Greene, Carl F. | en_US |
| dc.creator | Younger, John E. | en_US |
| dc.date.accessioned | 2016-05-25T18:51:14Z | |
| dc.date.available | 2016-05-25T18:51:14Z | |
| dc.date.created | 1930-08-30 | en_US |
| dc.date.issued | 1930-08-30 | en_US |
| dc.identifier.uri | http://hdl.handle.net/11200/48596 | |
| dc.description | This 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.format | en_US | |
| dc.publisher | Washington, D.C.: Chief of Air Corps | en_US |
| dc.relation.ispartofseries | Air Corps information circular (Aviation) ; v. 7, no. 653 | en_US |
| dc.relation.ispartofseries | Air Corps technical report ; Serial no. 3237 | en_US |
| dc.subject | Aeronautics--Research | en_US |
| dc.subject | Aeronautics--Systems engineering | en_US |
| dc.subject | Airplanes--Design and construction | en_US |
| dc.subject | Flutter (Aerodynamics) | en_US |
| dc.subject | Wind tunnel testing | en_US |
| dc.subject | Airplanes--Wings | en_US |
| dc.title | 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) | en_US |
| dc.type | Text | en_US |
| dc.relation.references | Study of Wing Flutter. Part I. Test of apparatus and discussion of procedure A.D.M. 1014 | en_US |
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