Double-decoupled inverse design of natural laminar flow nacelle under transonic conditions-Reference-Cited by-同舟云学术

Double-decoupled inverse design of natural laminar flow nacelle under transonic conditions

Published:2023-06 Issue:6 Volume:36 Page:1-18
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHANG Heng,LI Jie,YANG Zhao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

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4. Lynde MN, Campbell RL, Viken SA. Additional findings from the common research model natural laminar flow wind tunnel test. AIAA aviation 2019 forum. Reston: AIAA; 2019.

5. Key aerodynamic technologies for aircraft engine nacelles;Raghunathan;Aeronaut J,2006

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