Empirical measurements of small unmanned aerial vehicle co-axial rotor systems.
- Published version (with publisher's formatting)
Available under License Creative Commons Attribution-NoDerivatives.
Small unmanned aerial vehicles (SUAV) are beginning to dominate the area of intelligence, surveillance, target acquisition and reconnaissance (ISTAR) in forward operating battlefield scenarios. Of particular interest are vertical take-off and landing (VTOL) variants. Within this category co-axial rotor designs have been adopted due to their inherent advantages of size and power to weight ratio. The inter-rotor spacing attribute of a co-axial rotor system appears to offer insight into the optimum design characteristic. The H/D ratio has been cited as a significant factor in many research papers, but to date has lacked an empirical value or an optimal dimensionless condition. In this paper the H/D ratio of a SUAV has been explored thoroughly, reviewing the performance of these systems at incremental stages, the findings from this study have shown that a range of H/D ratios in the region of (0.41-0.65) is advantageous in the performance of SUAV systems. This finding lends itself to the theory of inter-rotor spacing as a non-dimensionally similar figure, which cannot be applied across a spectrum of systems; this could be attributed to the viscous losses of flight at low Reynolds Numbers (< 50,000).
|Research Areas:||A. > School of Science and Technology|
|Notes on copyright:||Open access journal|
|Depositing User:||Dr Stephen Prior|
|Date Deposited:||27 Jan 2011 12:47|
|Last Modified:||01 Oct 2015 16:33|
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