A ground vibration test was conducted on a Lockheed JetStar airplane that had been modified for the purpose of conducting laminar flow control experiments. The test was performed prior to initial flight flutter tests. Both sine-dwell and single-point-random excitation methods were used. The data presented include frequency response functions and a comparison of mode frequencies and mode shapes from both methods.
Ground vibration test of the laminar flow control JStar airplane
01.10.1985
Report
Keine Angabe
Englisch
Natural Laminar Flow and Airplane Stability and Control
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