Multidisciplinary Vehicle Shape and Trajectory Optimization for a Hypersonic Flight Experiment Using a Sounding Rocket
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/64/3/64_64_182/_pdf
Reference16 articles.
1. 1) Taguchi, H., Kobayashi, H., Kojima, T., Ueno, A., Imamura, S., Hongoh, M. and Harada, K.: Research on Hypersonic Aircraft Using Pre-Cooled Turbojet Engines, Acta Astronautica, 73 (2012), pp. 164-172.
2. 2) Smith, T. R., Bowcutt, K. G., Selmon, J. R., Mirranda, L., Northrop, B., Maris, R., Unger, E. R., Lau, K. Y., Silvester, T., Alesi, H., Paull, A., Paull, R. and Dolvin, D. J.: HIFiRE 4: A Low-Cost Aerodynamics, Stability, and Control Hypersonic Flight Experiment, AIAA Paper 2011-2275, 2011.
3. 3) Güulhan, A., Siebe, F., Thiele, T., Neeb, D., Turner, J. and Ettl, J.: Sharp Edge Flight Experiment-II Instrumentation Challenges and Selected Flight Data, J. Spacecraft Rockets, 51, 1 (2014), pp. 175-186.
4. 4) Pezzella, G., Marini, M., Cicala, M., Vitale, A., Langener, T. and Steelant, J.: Aerodynamic Characterization of HEXAFLY Scramjet Propelled Hypersonic Vehicle, AIAA Paper 2014-2844, 2014.
5. 6) Penland, J. A., Dillon, J. L. and Pittman, J. L.: An Aerodynamic Analysis of Several Hypersonic Research Airplane Concepts from $M = 0.2$ to 6.0, J. Aircraft, 15, 11 (1978), pp. 716-723.
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