Shock Control of a Low-Sweep Transonic Laminar Flow Wing-Reference-Cited by-同舟云学术

Shock Control of a Low-Sweep Transonic Laminar Flow Wing

Published:2019-06 Issue:6 Volume:57 Page:2408-2420
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhu Maolin¹,Li Yonghong²,Qin Ning³,Huang Yong²,Deng Feng⁴,Wang Yibin⁴,Zhao Ning⁴

Affiliation:

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

2. China Aerodynamics Research and Development Center, Mianyang 621000, People’s Republic of China

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

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

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.J058011

Reference37 articles.

1. KallasS.Geoghegan-QuinnM.DareckiM.EdelstenneC.EndersT.FernandezE.HartmanP. “Flightpath 2050 Europe’s Vision for Aviation,” European Commission, TR 98, Brussels, Belgium, 2011.

2. Gains in Fuel Efficiency: Multi-Stop Missions vs. Laminar Aircraft

3. AbbottI. H.Von DoenhoffA. E.StiversL. Jr. “Summary of Airfoil Data,” NACA TR-824, 1945.

4. SomersD. M. “Design and Experimental Results for a Natural-Laminar-Flow Airfoil for General Aviation Applications,” NASA TP-1865, 1981.

5. Observations and implications of natural laminar flow on practical airplane surfaces

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