Loose Fluid-Structure Coupled Approach for a Rotor in Descent Incorporating Fuselage Effects

A loose coupling approach is used to combine a comprehensive structural dynamics code CAMRAD II and a computational fluid dynamics solver KFLOW to validate the data and to identify the effect of fuselage on the aeroelastic behavior of the second higher harmonic rotor acoustic test rotor. The computa...

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Veröffentlicht in:	Journal of aircraft 2013-07, Vol.50 (4), p.1016-1026
Hauptverfasser:	Jung, Sung Nam, Sa, Jeong Hwan, You, Young Hyun, Park, Jae Sang, Park, Soo Hyung
Format:	Artikel
Sprache:	eng
Schlagworte:	Acoustic tests Aerodynamics Aeroelasticity Air transportation and traffic Aircraft Airframes Applied sciences Computational fluid dynamics Correlation Dynamics Exact sciences and technology Fluid dynamics Fuselages Ground, air and sea transportation, marine construction Mathematical models Miss distance Rotors Upwash Velocity distribution Vorticity
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