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Journal: Aerospace, 2024
Volume: 11
Number: 233

Article: Derivation and Flight Test Validation of Maximum Rate of Climb during Takeoff for Fixed-Wing UAV Driven by Propeller Engine
Authors: by Katsumi Watanabe, Takuma Shibata and Masazumi Ueba
Link: https://www.mdpi.com/2226-4310/11/3/233

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