Stability Analysis of Tailsitters in Vertical Takeoff and Landing Flights-Reference-Cited by-同舟云学术

Stability Analysis of Tailsitters in Vertical Takeoff and Landing Flights

Published:2019-07 Issue:4 Volume:56 Page:1487-1500
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wang Xiangyang¹,Yuan Xiaming¹,Zhu Jihong¹,Yang Yunjie¹

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Aeronautical Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035209

Reference20 articles.

1. PowellM. L. Jr.KirbyR. H.SmithC. C. Jr. “Flight Investigation of the Stability and Control Characteristics of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane During Constant-Altitude Transitions,” NACA RM SL53E18, 1953.

2. SuttonF. B.BuellD. A. “The Effect of an Operating Propeller on the Aerodynamic Characteristics of a 1/10-Scale Model of the Lockheed XFV-1 Airplane at High Subsonic Speeds,” NACA RM SA52E06, 1952.

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