Publikationsdatum:
2019-06-28
Beschreibung:
A mathematical model of the Sikorsky SH-3G helicopter based on classical nonlinear, quasi-steady rotor theory was developed. The model was validated statically and dynamically by comparison with Navy flight-test data. The model incorporates ad hoc revisions which address the ideal assumptions of classical rotor theory and improve the static trim characteristics to provide a more realistic simulation, while retaining the simplicity of the classical model.
Schlagwort(e):
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Materialart:
NASA-TM-84316
,
A-9187
,
NAS 1.15:84316
Format:
application/pdf
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