Mitigation of Pusher-Propeller Installation Effects by Pylon Trailing-Edge Blowing-Reference-Cited by-同舟云学术

Mitigation of Pusher-Propeller Installation Effects by Pylon Trailing-Edge Blowing

Published:2017-01 Issue:1 Volume:54 Page:292-300
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sinnige Tomas¹,Ragni Daniele¹,Eitelberg Georg¹,Veldhuis Leo L. M.¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C034000

Reference16 articles.

1. PageM. A.IveyD. M.WelgeH. R. “Ultra High Bypass Engine Applications to Commercial and Military Aircraft,” Aerospace Technology Conference & Exposition, SAE TP-861720, Oct. 1986. doi:10.4271/861720

2. Pressure-time history of pylon wake on a pusher propeller in flight

3. Pressure-time history of pylon wake on a pusher propeller in flight

4. Frequency-domain analysis of fluctuating pressure on a pusher propeller blade surface

5. Progress in aerodynamic and aeroacoustic integration of CROR propulsion systems

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