Error Analysis for CAMUI Type Hybrid Rocket Regression Simulation
Author:
Affiliation:
1. Graduate School of Engineering, Division of Mechanical and Space Engineering, Hokkaido University
2. Faculty of Engineering, Hokkaido University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/17/4/17_17.519/_pdf
Reference3 articles.
1. 1) Nagata, H., Hagiwara, S., Kaneko, Y., Wakita, M., Totani, T., and Uematsu, T.: Development of Regression Formulas for CAMUI Type Hybrid Rocket as Function of Local O/F, AIAA Paper 2010-7117.
2. 2) Nagata, H: Development of a Liquid Oxygen Supply System for a Small-scale Sounding Rocket, Japanese Journal of Multiphase Flow, 27 (2013), pp.393-400 (in Japanese).
3. 3) Nagata, H., Nohara, M., Kanai, R., Wakita, M., and Totani, T.: Effects of Reynolds Number and Flow Channel Geometry on Fuel Regression Characteristics in CAMUI Type Hybrid Rocket, 36th IAC, Naples,Italy, IAC-12-C4.9.5, 2006.
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