Various measurements concerning unsteady aerodynamics are discussed. The unsteady pressure measurements in a wing, used as points of comparison for the unsteady aerodynamic computation methods on which flutter computations are based, are mentioned and wind tunnel tests of flutter are analyzed. Various measurements, their use, and the safety systems are discussed to give an overview of what can be done in this area.
Unsteady Wind Tunnel Tests
1992
38 pages
Report
Keine Angabe
Englisch
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