1. 1) Yoshida, K.: Supersonic Drag Reduction Technology in the Scaled Supersonic Experimental Airplane Project by JAXA, Progr. Aerospace Sci., 45 (2009), pp. 124-146.
2. 2) Ohnuki, T., Hirako, K. and Sakata, K.: National Experimental Supersonic Transport Project, International Congress of the Aeronautical Science, 2006-1.4.1, AIAA J., 10 (2006), pp. 1441-1447.
3. 3) Ueda, Y., Ishikawa, H. and Yoshida, K.: Three Dimensional Boundary Layer Transition Analysis in Supersonic Flow Using a Navier-Stokes Code, Proceedings of ICAS 2004-2.8.2, on CD-ROM, 2004.
4. 4) Arnal, D.: Boundary Layer Transitions: Predictions Based on Linear Theory, AGARD Report 793, 1994, pp. 2/1-63.
5. 5) Joslin, R. D., Horta, L. G. and Chen, F.: Transitioning Active Flow Control to Applications, AIAA Paper 99-3575, 1999.