Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions-Reference-Cited by-同舟云学术

Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions

Published:2014-06 Issue:6 Volume:52 Page:1294-1306
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ueda Yoshine¹,Yoshida Kenji²,Matsushima Kisa³,Ishikawa Hiroaki⁴

Affiliation:

1. Aviation Program Group, Tokyo Business Service Co. Ltd., Tokyo 160-0023, Japan

2. Aviation Program Group, Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan

3. Mechanical Engineering and Sciences, University of Toyama, Toyama 930-8555, Japan

4. Aviation Program Group, Sankosoft Co. Ltd., Tokyo 169-0075, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052555

Reference12 articles.

1. Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA

2. Inverse design method for wings of supersonic transport

3. Transition Measurements on the Natural Laminar Flow Wing at Mach 2

4. ArnalD. “Boundary Layer Transition: Predictions Based on Linear Theory,” AGARD FDP/VKI Special Course on Progress in Transition Modeling, AGARD, Rept. 793, 1993.

Cited by 19 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Attenuation of boundary-layer instabilities for natural laminar flow design on supersonic highly swept wings;Chinese Journal of Aeronautics;2024-07

2. Recent progress of efficient low-boom design and optimization methods;Progress in Aerospace Sciences;2024-04

3. Natural Laminar Flow Design for Highly Swept Wings;Lecture Notes in Electrical Engineering;2022-08-31

4. Effects of Atmospheric Profiles on Sonic Boom Perceived Level from Supersonic Vehicles;AIAA Journal;2021-12

5. Conceptual aerodynamic design of an executive supersonic passenger aircraft – ESPA;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-06-07