Alleviation of Propeller-Slipstream-Induced Unsteady Pylon Loading by a Flow-Permeable Leading Edge-Reference-Cited by-同舟云学术

Alleviation of Propeller-Slipstream-Induced Unsteady Pylon Loading by a Flow-Permeable Leading Edge

Published:2019-05 Issue:3 Volume:56 Page:1214-1230
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sinnige Tomas¹,Corte Biagio Della¹,De Vries Reynard¹,Avallone Francesco¹,Merino-Martínez Roberto¹,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

https://arc.aiaa.org/doi/pdf/10.2514/1.C035250

Reference39 articles.

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2. Advanced propulsion through the 1990s - An airframer's view

3. Ultra High Bypass Engine Applications to Commercial and Military Aircraft

4. Potential benefits for propfan technology on derivatives of future short- to medium-range transport aircraft

5. GoldsmithI. M. “A Study to Define the Research and Technology Requirements for Advanced Turbo/Propfan Transport Aircraft,” NASA CR-166138, Feb. 1981.

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