Higher-Order Free-Wake Method for Propeller–Wing Systems-Reference-Cited by-同舟云学术

Higher-Order Free-Wake Method for Propeller–Wing Systems

Published:2019-01 Issue:1 Volume:56 Page:150-165
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Cole Julia A.¹,Maughmer Mark D.²,Kinzel Michael²,Bramesfeld Götz³

Affiliation:

1. Bucknell University, Lewisburg, Pennsylvania 17837

2. Pennsylvania State University, University Park, Pennsylvania 16802

3. Ryerson University, Toronto, Ontario M5B 2K3, Canada

Funder

Penn State Vertical Lift Research Center of Excellence

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034720

Reference56 articles.

1. Performance and Design Investigation of Heavy Lift Tilt-Rotor with Aerodynamic Interference Effects

2. RaymerD. P.WilsonJ.PerkinsD.RizziA.ZhangM.Ramirez PuentesA. “Advanced Technology Subsonic Transport Study: N+3 Technologies and Design Concepts,” NASA TM-217130, 2011.

3. Drag Reduction Through Distributed Electric Propulsion

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