Benefit Assessment of Low-Sweep Transonic Natural Laminar Flow Wing for Commercial Aircraft-Reference-Cited by-同舟云学术

Benefit Assessment of Low-Sweep Transonic Natural Laminar Flow Wing for Commercial Aircraft

Published:2021-11 Issue:6 Volume:58 Page:1294-1301
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Fan Zhouwei¹,Yu Xiongqing¹,Qin Ning²^ORCID,Zhu Maolin¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

2. The University of Sheffield, Sheffield, England S1 3JD, United Kingdom

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036138

Reference41 articles.

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2. GreitzerE. M.BonnefoyP. A.De la Rosa BlancoE.DorbianC. S.DrelaM.HallD. K.HansmanR. J.HilemanJ. I. “N+3 Aircraft Concept Designs and Trade Studies, Final Report: Volume 1,” NASA CR-2010-216794/VOL1, 2010.

3. Building the future aircraft design for the next century

4. FischerM. C.AshR. L. “A General Review of Concepts for Reducing Skin Friction, Including Recommendations for Future Studies,” NASA TM-X-2894, 1974.

5. JoslinR. D. “Overview of Laminar Flow Control,” NASA TP-1998-208705, 1998.

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