Designing Wing Twist or Planform Distributions for Specified Lift Distributions
نویسندگان
چکیده
منابع مشابه
Lift Superposition and Aerodynamic Twist Optimization for Achieving Desired Lift Distributions
A method for achieving an arbitrary lift distribution with an arbitrary planform is presented. This is accomplished through optimizing aerodynamic twist for a given number of either known airfoils or airfoils to be designed. The spanwise locations of these airfoils are optimized to get as close to the desired lift distribution as possible. Airfoils are linearly interpolated between these points...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2019
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.c035206