Experimental and numerical results of a propeller of 0.3 m diameter operated at 5000 RPM
and axial velocity ranging from 0 to 20 m/s and advance ratio ranging from 0 to 0.8 are …

The increasing use of unmanned aerial vehicles and micro air vehicles creates a strong
demand for the accurate aerodynamic performance of small-diameters fixed-pitch …

Analyzing the propeller aerodynamic performance is of vital importance for research and
improvement of unmanned aerial vehicles. This paper presents the design requirements for …

The concept and preliminary design of an unmanned lighter-than-air (LTA) platform
instrumented with different remote sensing technologies is presented. The aim is to assess …

View Video Presentation: https://doi. org/10.2514/6.2021-2598. vid In aircraft conceptual
design, a fast and robust model for rotor aerodynamic analysisis valuable. A commonly used …

Summary Unmanned Aircraft Systems (UAS) are state of the art in aerospace industry for
both commercialandmilitaryapplications. Inparticular, smallscalemulticoptershavegained …

The commercially available unmanned aerial vehicles are not good enough for search and
rescue flight at high altitudes. This is because as the altitude increases, the density of air …

Experimental and numerical results of a propeller of 0.3 m diameter operated in quiescent
standard ambient conditions at 5000 RPM and axial velocity ranging from 0 to 20 m/s and …

A whirling arm is an effective device to measure propeller characteristics at low advance
ratios. In the authors' preceding research, an apparent advance ratio was adopted to …

With the advent of quadrotor unmanned aerial vehicles (UAV) becoming more prevalent for
military and commercial applications, gaining a better understanding of their aerodynamic …