1. 1) Honda, M. and Yoshida, K.:D-SEND Project for Low Sonic Boom Design Technology, Proceedings of 28th Congress of International Council of the Aeronautical Science, Brisbane, September 23-28, 2012-1.2.1, [CD-ROM] ,2012.
2. 2) Yoshida, K., Kwak, D. Y., Tokugawa, N. and Ishikawa, H.: Concluding Report of Flight Test Data Analysis on the Supersonic Experimental Airplane of NEXST Program by JAXA, Proceedings of 27th Congress of International Council of the Aeronautical Science, Nice, September 19-24, 2010-2.8.2, [CD-ROM], 2004.
3. 3) Tokugawa, N., Kwak, D. Y., Yoshida, K. and Ueda, Y.: Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1, Journal of Aircraft, 45, 2008, pp. 1495-1504.
4. 4) Dodbele, S. S., van Dam, C.P. and Vijgen P. M. H. W.: Design of Fuselage Shapes for Natural Laminar Flow, NASA CP-3970, 1986.
5. 5) Fujino, M.: Development of Honda Jet, Proceedings of 24th Congress of International Council of the Aeronautical Science, Yokohama, August 29- September 3, 2004-1.7.2 (I.L.), [CD-ROM], 2004.