کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1719216 1520165 2014 51 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics
ترجمه فارسی عنوان
کاهش نظم ناپیوسته مدل سازی آیرودینامیک برای تحلیل ثبات و کنترل با استفاده از دینامیک سیالات محاسباتی
کلمات کلیدی
آیرودینامیک ناپایدار، دینامیک سیالات محاسباتی، مدل سفارش کاهش یافته، توابع رسمی، توابع پایه شعاعی، توابع ولتررا
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی

Recent advances and challenges in the generation of reduced order aerodynamic models using computational fluid dynamics are presented. The models reviewed are those that can be used for aircraft stability and control analysis and include linear and nonlinear indicial response methods, Volterra theory, radial basis functions, and a surrogate-based recurrence framework. The challenges associated with identification of unknowns for each of the reduced order methods are addressed. A range of test cases, from airfoils to full aircraft, have been used to evaluate and validate the reduced order methods. The motions have different amplitudes and reduced frequencies and could start from different flight conditions including those in the transonic speed range. Overall, these reduced order models help to produce accurate predictions for a wide range of motions, but with the advantage that model predictions require orders of magnitude less time to evaluate once the model is created.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Progress in Aerospace Sciences - Volume 71, November 2014, Pages 167–217
نویسندگان
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