Low Reynolds Number Rotor Blade Aerodynamic Analysis

Tulwin, T

Tulwin, T (reprint author), Lublin Univ Technol, Dept Thermodynam Fluid Mech & Aircraft Prop, Nadbystrzycka 38D, PL-20618 Lublin, Poland.

III INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN ENGINEERING SCIENCE (CMES 18), 2019; 252 ():

Abstract

Maintaining a steady hover flight in a rotorcraft usually requires high energy input. The aim of the paper is to prove that it is possible to vastly r......

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