Transitional Strategy for Annular Lift Fan Aircraft to Lower the Momentum Drag and Pitching Moment-Reference-Cited by-同舟云学术

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Transitional Strategy for Annular Lift Fan Aircraft to Lower the Momentum Drag and Pitching Moment

Published:2021-03 Issue:2 Volume:34 Page:04021002
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jiang Yun¹,Zhang Bo²

Affiliation:

1. Senior Engineer, UAV Research Institute, Northwestern Polytechnical Univ., 127 West Youyi Rd., Xi’an 710072, China (corresponding author).

2. Senior Engineer, UAV Research Institute, Northwestern Polytechnical Univ., 127 West Youyi Rd., Xi’an 710072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001242

Reference23 articles.

1. Tip Clearance Investigation of a Ducted Fan Used in VTOL Unmanned Aerial Vehicles—Part I: Baseline Experiments and Computational Validation

2. Genesis of the F-35 Joint Strike Fighter

3. Fleming J. T. Jones J. Lusardi P. Gelhausen and D. Enns. 2004. “Improved control of ducted fan VTOL UAVs in crosswind turbulence.” In Vol. 152 of Proc. AHS 4th Decennial Specialist’s Conf. on Aeromechanics 1–12. Fairfax VA: American Helicopter Society.

4. Graf W. 2005. “Effects of duct lip shaping and various control devices on the hover and forward flight performance of ducted fan UAVs.” Master’s thesis Dept. of Aerospace Engineering Virginia Tech.

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