An Innovative UAV Design

Author:

Nietz Thomas1,Baber S.1

Affiliation:

1. Northrop Grumman Corporation

Publisher

American Institute of Aeronautics and Astronautics

Reference3 articles.

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Performance Characteristics of Fluidic-Based Thrust Augmentation Using a Slot Jet for Unmanned Aerial Vehicle Propulsion;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

2. Analysis on the Power Characteristics of Lift-Fan VTOL;Applied Mechanics and Materials;2011-07

3. Analysis on the Transition Mode of Lift-Fan VTOL;Applied Mechanics and Materials;2011-07

4. Co-flow Fluidic Thrust Vectoring Requirements for Longitudinal and Lateral Trim Purposes;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

5. Dynamic Stability Study of a Conceptual Fluidic Thrust-Vectored Aerial Tail-sitter;AIAA Modeling and Simulation Technologies Conference and Exhibit;2006-06-15

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