Effect of inlet distortion with crosswind on aircraft-engine intake aerodynamic performance-Reference-Cited by-同舟云学术

Effect of inlet distortion with crosswind on aircraft-engine intake aerodynamic performance

Published:2022 Issue:910 Volume:88 Page:21-00357-21-00357
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

NARUSE Hiroki¹,ISHII Tatsuya²,OINUMA Hideshi²,KUSUDA Shinya³,OOBA Yoshinori³,HIRAKAWA Karin³,AONO Hikaru⁴,ISHIKAWA Hitoshi⁵

Affiliation:

1. Department of Mechanical Engineering, Graduate School of Engineering, Tokyo University of Science

2. Japan Aerospace Exploration Agency

3. IHI Corporation

4. Department of Mechanical Engineering and Robotics, Shinshu University

5. Department of Mechanical Engineering, Tokyo University of Science

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/88/910/88_21-00357/_pdf

Reference15 articles.

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2. Feiler, C. E. and Groeneweg, J. F., Summary of forward velocity effects on fan noise, AIAA 1977-1319 (1977).

3. Hall, C.A. and Hynes, T.P., Nacelle interaction with natural wind before takeoff, Journal of Propulsion and Power, Vol.21, No.5(2005), pp.784-791.

4. Hall, C.A. and Hynes, T.P., Measurements of intake separation hysteresis in a model fan and nacelle rig, Journal of Propulsion and Power, Vol.22, No.4(2006), pp.872-879.

5. Ishii, T., Nagai, K., Oinuma, H., Kagaya, R. and Oishi, T., Experimental study on acoustic performances of notched nozzle using to a subscale turbofan engine, ASME-GT2018-76713(2018).