کتابخانه دیجیتال دانشگاه هنر اصفهان | Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight.

Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight.

نام

Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight.

زبان اثر

انگلیسی

شناسگر

10.1007/s00158-004-0469-x (شماره مدرک)

10.1007_s00158-007-0137-z (importid)

ناشر

تاریخ انتشار

2008

قالب (کتاب)

کتاب