Performance Analysis of Aircraft with Laminar Flow Control System Based on Conceptual Design Method
Author:
Affiliation:
1. The University of Tokyo
2. presently Toyota Central R&D Labs., Inc.
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/astj/17/0/17_JSASS-D-17-00061/_pdf
Reference18 articles.
1. 3) Lehner, S. and Crossley, W.: Combinational Optimization to Include Greener Technologies in a Short-to-medium Range Commercial Aircraft, 26th International Congress of the Aeronautical Sciences, ICAS-2008-4.10.2, Anchorage, 2008.
2. Aircraft Conceptual Design Method Considering Secondary Power Systems Effect on Aircraft Performance
3. 5) Shibata, K., Maedomari, T., Rinoie, K., Morioka, N. and Oyori, H.: Aircraft Secondary Power System Integration into Conceptual Design and Its Application to More Electric System, SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, Paper No. 2014-01-2199, 2014.
4. 7) Saric, W.S. and Reed, H.L.: Toward Practical Laminar Flow Control- Remaining Challenges, 2nd AIAA Flow Control Conference, AIAA 2004-2311, 2004.
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