Integration, Testing and Validation, of a Small Hybrid-Electric Remotely-Piloted Aircraft

JK Ausserer - 2012 - scholar.afit.edu
Parallel hybrid-electric technology offers a wide variety of new mission capabilities including
low-observable loiter operations and increased fuel efficiency for small remotely-piloted …

An experimental investigation into the effects of atmospheric turbulence on the aerodynamics of micro air vehicle wings

B Loxton - 2011 - researchrepository.rmit.edu.au
An Experimental Investigation into the Effects of Atmospheric Turbulence on the
Aerodynamics of Micro Air Vehicle Wings Page 1 An Experimental Investigation into the …

[PDF][PDF] Design, fabrication and testing of flapping wing micro air vehicle

K Sai, K Bharadwaj, KR Teja, K Dagamoori… - Int. J. Eng. Res …, 2016 - academia.edu
Flapping flight has the potential to revolutionize micro air vehicles (MAVs) due to increased
aerodynamic performance, improved maneuverability and hover capabilities. The purpose …

[PDF][PDF] The small scales of turbulence in atmospheric winds at heights relevant to MAVs

M Thompson - School of Aerospace, Mechanical and Manufacturing …, 2012 - core.ac.uk
Summary Micro Air Vehicles (MAVs) are typically of low mass and moment of inertia and
have flight speeds comparable to birds and larger insects. Such craft traverse the lower …

Experimental performance evaluation of coaxial rotors for a micro aerial vehicle

P Singh, C Venkatesan - Journal of aircraft, 2013 - arc.aiaa.org
Because of their potential for application in both civil and military sectors as well as the
challenge in designing a tiny flying vehicle, micro aerial vehicles have attracted enormous …

Proper orthogonal decomposition analysis of an airfoil performances under a small vortical gust

MM Oueslati, AW Dahmouni… - Journal of Applied Fluid …, 2022 - jafmonline.net
This paper investigates the performance of a non-symmetric airfoil in a perturbed flow for a
low Reynolds number by creating small vortical structures. A newly designed two …

Suction control of flow separation of a low-aspect-ratio wing at a low Reynolds number

Z Zhi-yong, Z Wang-long, C Zhi-hua… - Fluid Dynamics …, 2018 - iopscience.iop.org
Suction-based flow control is explored as one of means of enhancing the performance of a
low aspect ratio (AR) wing. Large-eddy simulation (LES) was performed to investigate the …

Review of self-induced roll oscillations and its attenuation for low-aspect-ratio wings

T Hu - Proceedings of the Institution of Mechanical Engineers …, 2019 - journals.sagepub.com
Micro aerial vehicles are currently receiving growing interest because of their broad
applications in many fields. In their flight tests, the onset of unwanted large amplitude roll …

The airfoil design and parameter optimization of the deformable micro air vehicle

S Huang, H Qiu, Y Wang - Engineering Computations, 2023 - emerald.com
Purpose Since most of the existing literature do not disclose the node coordinate data of its
fixed-wing aircraft airfoil, in order to develop and obtain a practical and suitable deformation …

The suppression of flying-wing roll oscillations with open and closed-loop spanwise blowing

Y Dong, Z Shi, K Chen, S Tong, D Wei - Aerospace Science and …, 2020 - Elsevier
Uncommanded self-induced roll oscillations cause significant challenges in flight control
and are ubiquitous in high-attack-angle flights in the flying-wing configuration. Spanwise …