Modeling and Transition Flight Control of Distributed-Propulsion-Wing Vtol Uav with Induced Wing Configuration

Author:

Zhao Qingfeng,Zhou Zhou,Wang Rui

Publisher

Elsevier BV

Reference41 articles.

1. Aero-Propulsive and Propulsor Cross-Coupling Effects on a Distributed Propulsion System;A T Perry;AIAA Aerospace Sciences Meeting,2018

2. Wing Structure of the Next-Generation Civil Tiltrotor: From Concept to Preliminary Design;M Belardo;Aerospace,2021

3. Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight;R De Vries;Aerospace Science and Technology,2021

4. Series-hybridisation, distributed electric propulsion and boundary layer ingestion in long-endurance, small remotely piloted aircraft: Fuel consumption improvements;A O Tiseira Izaguirre;Aerospace Science and Technology,2022

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