Preprints
https://doi.org/10.5194/egusphere-2026-977
https://doi.org/10.5194/egusphere-2026-977
19 Mar 2026
 | 19 Mar 2026
Status: this preprint is open for discussion and under review for Atmospheric Measurement Techniques (AMT).

Aerodynamic evaluation of wind speed sensor placement on UAVs for meteorological applications

Ashish Pastay, Shrivathsan Narayanan, and Bharath Govindarajan

Abstract. Vertical takeoff and landing Unmanned Aerial Vehicles (VTOL-UAVs) can provide accurate, highly resolved, and repeatable atmosphere measurements, especially in scenarios where conventional measurement techniques are inadequate, or impractical. Wind estimation using UAV-mounted sensors is significantly influenced and contaminated by rotor-induced flows, making its placement a critical design consideration for meteorological measurements. This work investigates optimal locations for wind speed sensor placement on various UAV systems by studying the rotor-induced flow field using a free-vortex wake model (FVM) across a single-rotor, quad-rotor, and hexa-rotor configurations under hover, axial descent, and forward-descent flight conditions. This model is validated with an in-house experimental setup for velocity measurements. Care is taken to ensure these results are applicable across a wide range of practical UAV operating conditions through the dimensional disk loading (DL) parameter. The rotor-induced velocity fields are evaluated on multiple planes perpendicular to the rotor disk, and "quiet-zones" for sensor placement are identified based on a threshold of 1% rotor-tip speed. Results reveal that the location and extent of the quiet-zones are strongly dependent on the flight condition. For single-rotor in hover, a well-defined quiet-zone exists above the rotor disk, while viable sensor placement locations are substantially reduced in axial descent. Forward descent introduces asymmetric wake skew, limiting quiet-zones to the upstream, at smaller axial distances. For multi-rotor configurations, the system geometric center is particularly suitable for sensor placement, compared to axial locations about the individual rotor hubs. Overall, by analyzing various rotor systems in different flight conditions, the present work provides a practical guidance for the design of accurate UAV-based atmospheric measurement systems.

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Ashish Pastay, Shrivathsan Narayanan, and Bharath Govindarajan

Status: open (until 24 Apr 2026)

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Ashish Pastay, Shrivathsan Narayanan, and Bharath Govindarajan
Ashish Pastay, Shrivathsan Narayanan, and Bharath Govindarajan
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Latest update: 19 Mar 2026
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Short summary
Multi-rotor drones are increasingly being used to measure wind and atmospheric conditions, but their rotors disturb the surrounding air, affecting sensor accuracy. We used an experimentally validated numerical model to identify zones of minimal rotor influence, on various drone configurations. Sensors can be placed above the rotors in hover, while descent and forward descent conditions are more restrictive. Overall, these findings provide practical guidance for wind sensor placement on drones.
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