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 JetStar Airplane
1985
61 pages
Report
No indication
English
Online Contents | 2007
SAE Technical Papers | 1961
|Engineering Index Backfile | 1961
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