A Nomad aileron was modified by the addition of strain gauges and associated wiring, to permit its use in loads-measurement trials. This modification rendered the aileron non-standard, so a flight flutter trial was conducted to verify the aeroelastic stability of the loads aircraft when fitted with this aileron. This report describes the flight flutter trial and presents the results.
Flight Flutter Test of a Nomad N24A Aircraft Fitted with One Modified Aileron
1995
37 pages
Report
No indication
English
Engineering Index Backfile | 1943
|Composite Flight Test Boom for NOMAD N22b Aircraft
NTIS | 1981
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