Validation of a Wind Tunnel Propeller Dynamometer for Group 2 Unmanned Aircraft

Validation of a Wind Tunnel Propeller Dynamometer for Group 2 Unmanned Aircraft

This paper presents an approach to validate a wind tunnel propeller dynamometer applicable to Group 2 unmanned aircraft. The intended use of such a dynamometer is to characterize propellers over a relevant range of sizes and operating conditions, under which such propellers are susceptible to low-Re...

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Bibliographic Details
Main Authors: Muwanika Jdiobe, Kurt Rouser, Ryan Paul, Austin Rouser
Format: Article
Language:English
Published: MDPI AG 2022-09-01
Series:Applied Sciences
Subjects:
propeller
propulsion
UAS
dynamometer
thrust
pitch
Online Access:https://www.mdpi.com/2076-3417/12/17/8908

Internet

https://www.mdpi.com/2076-3417/12/17/8908

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