کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
762515 896697 2011 15 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Aerodynamic shape optimization of hovering rotor blades using a Non-Linear Frequency Domain approach
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
پیش نمایش صفحه اول مقاله
Aerodynamic shape optimization of hovering rotor blades using a Non-Linear Frequency Domain approach
چکیده انگلیسی

This paper presents a discrete adjoint-based aerodynamic optimization algorithm for helicopter rotor blades in hover using a Non-Linear Frequency Domain approach. The procedure to be used can be broken down into two phases: first, investigate and develop an accurate inviscid numerical model for the current generation of helicopter rotor blades; and second, demonstrate the approach for the redesign of a transonic Caradonna–Tung two-bladed rotor. The results in determining the optimum aerodynamic configurations require an objective function which minimizes the inviscid torque coefficient and maintains the desired thrust level at transonic conditions.


► Validated the Non-Linear Frequency Domain method for Rotorcraft Flows.
► Developed the Discrete Adjoint Equations for the Non-Linear Frequency Domain method.
► Demonstrated aerodynamic shape optimization to improve the performance of hovering rotor blades.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Computers & Fluids - Volume 51, Issue 1, 15 December 2011, Pages 1–15
نویسندگان
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