Double-Ducted Fan as an Effective Lip Separation Control Concept for Vertical-Takeoff-and-Landing Vehicles-Reference-Cited by-同舟云学术

Double-Ducted Fan as an Effective Lip Separation Control Concept for Vertical-Takeoff-and-Landing Vehicles

Published:2022-01 Issue:1 Volume:59 Page:233-252
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Akturk Ali¹^ORCID,Camci Cengiz¹

Affiliation:

1. The Pennsylvania State University, University Park, Pennsylvania 16802

Funder

National Rotorcraft Technology Center

PSU Vertical Lift Center of Excellence

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036386

Reference19 articles.

1. McCormickB. W., Aerodynamics of V/STOL Flight, Dover, New York, 1999, p. 245.

2. GrafW. E. “Effects of Duct Lip Shaping and Various Control Devices on the Hover and Forward Flight Performance of Ducted Fan UAVs,” Master’s Thesis, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 2005.

3. MortK. W.GamseB. “A Wind Tunnel Investigation of a 7-Foot-Diameter Ducted Propeller,” NASA TND-4142, 1967.

4. MortK. W.YaggyP. F. “Aerodynamic Characteristics of a 4-Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing,” NASA TND-1301, 1962.

5. YaggyP. F.MortK. W. “A Wind-Tunnel Investigation of a 4-Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing,” NASA TND-776, 1961.

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