Whirl flutter analysis of the commuter aircraft aeroelastic model wing -- engine component
Abstract eng: The submitted paper deals with whirl flutter of turboprop aircraft. It gives a summary of the airworthiness regulations requirements and the theoretical background concerning the mentioned aeroelastic phenomenon. The whirl flutter analysis was performed by means of the NASTRAN program system supported by other specialized software packages. The analysis was made on an aeroelastic model of the wing – engine component of a commuter aircraft for 40 passengers.
Publisher:
Institute of Theoretical and Applied Mechanics, AS CR, v.v.i., Prague
Conference Title:
Conference Title:
ENGINEERING MECHANICS 2006
Conference Venue:
Svratka (CZ)
Conference Dates:
2006-05-15 / 2006-05-18
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2014-11-12, last modified 2014-11-18
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