Multidisciplinary Design Optimization of Long or Short Range Hypersonic Aircraft

Author:

MATSUNO Yoshinori,TSUCHIYA Takeshi,IMAMURA Shunsuke,TAGUCHI Hideyuki

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference19 articles.

1. 1) Werner-Westphal, C., Heinze, W. and Horst, P.: Multidisciplinary Integrated Preliminary Design Applied to Unconventional Aircraft Configurations, J. Aircraft, 45 (2008), pp. 581–590.

2. 2) Tsuchiya, T. and Mori, T.: Optimal Design of Two-Stage-to-Orbit Space Planes with Airbreathing Engines, J. Spacecraft Rockets, 42 (2005), pp. 90–97.

3. 3) Yokoyama, N., Suzuki, S., Tsuchiya, T., Taguchi, H. and Kanda, T.: Multidisciplinary Design Optimization of Space Plane Considering Rigid Body Characteristics, J. Spacecraft Rockets, 44 (2007), pp. 121–131.

4. 4) McNamara, J. J. and Friedmann, P. P.: Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future, AIAA J., 49 (2011), pp. 1089–1122.

5. 5) Grant, M. J., Clark, I. G. and Braun, R. D.: Rapid Simultaneous Hypersonic Aerodynamic and Trajectory Optimization Using Variational Methods, AIAA Paper 2011-6640, 2011.

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