Derivation and Flight Test Validation of Maximum Rate of Climb during Takeoff for Fixed-Wing UAV Driven by Propeller Engine.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Mar2024, Vol. 11 Issue 3, p233, 14p
- Subject
PROPELLERS FLIGHT testing ENGINES DRONE aircraft TURBOPROP airplanes AIR speed - Language
- ISSN
- 22264310