Aerodynamic performance of a characteristic airfoil at low-Reynolds number and transonic flow under Mars sand-containing environment
The propeller tip of an unmanned aerial vehicle on Mars operates at a low-Reynolds
number (Re= 1–5× 10 4) and transonic velocity range (Ma= 0.7–1.2). Generally, this implies …
number (Re= 1–5× 10 4) and transonic velocity range (Ma= 0.7–1.2). Generally, this implies …