Development of Inverse Design System for Supersonic Natural Laminar Flow Wing on High Reynolds Number Condition

Author:

ISHIKAWA Hiroaki,TOKUGAWA Naoko,UEDA Yoshine,ITO Keigo,YOSHIDA Kenji

Publisher

Japan Society for Aeronautical and Space Sciences

Reference21 articles.

1. 1) König, L. and Hellstrom, T.: The Clean Sky Smart Fixed Wing Aircraft Integrated Technology Demonstrator: Technology Targets and Project Status, Proceedings of International Congress of the Aeronautical Science, 2010-5.9.3, 2010.

2. 2) Collier, F., Thomas, R., Burley, C., Nickol, C., Lee, C. and Tong. M.: Environmentally Responsible Aviation-Real Solutions for Environmental Challenges Facing Aviation, Proceedings of International Congress of the Aeronautical Science, 2010-1.6.1, 2010.

3. 3) Woo, G. and Glezer A.: Transition Control of Separating Flow over a Dynamically-Pitching Airfoil, AIAA Paper 2010-0861, 2010.

4. 4) Marshall, L. A.: Boundary-Layer Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment, NASA TM-1999-209013, 1999.

5. 6) Sturdza, P.: Extensive Supersonic Natural Laminar Flow on the Aerion Business Jet, AIAA Paper 2007-0685, 2007.

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