A Horizontal-Pendulum Type Thrust Stand for Evaluating Higher Frequency Variation by Applying Acceleration Measurement to Null-Balance Method-Reference-Cited by-同舟云学术

A Horizontal-Pendulum Type Thrust Stand for Evaluating Higher Frequency Variation by Applying Acceleration Measurement to Null-Balance Method

Published:2019 Issue:2 Volume:17 Page:175-180
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

YAMAUCHI Yusuke¹,YANO Yasuyuki²,KAKAMI Akira¹

Affiliation:

1. Department of Mechanical Design Systems Engineering, University of Miyazaki

2. Technical Center, University of Miyazaki

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/17/2/17_17.175/_pdf

Reference6 articles.

1. 1) George, P. S. and Oscar, B.: Rocket Propulsion Elements, John Wiley & Sons, New York, 2010, pp. 14-22.

2. 2) Kakami, A., Kashihara, K., Takeshida, S. and Yano, Y.: A New Thrust Measurement Method for Evaluating Higher Frequency Variation by Applying Acceleration Measurement to Null-balance Method, Trans. JSASS Aerospace Tech. Japan, 14, ists30 (2015), pp. Pb_123-Pb_130.

3. 3) Kakami, A., Hiyamizu, R., Masaki, S. and Tachibana, T.: A Preliminary Study on an Active-controlled Thrust Stand for Thrust Variation Measurement, Trans. JSASS Aerospace Technology Japan, ists25 (2006), pp. 212-217.

4. 4) Kakami, A. and Tachibana, T.: Thrust Evaluation in Wide Frequency Range using Active Control and Disturbance Observer, J. Propulsion and Power, 29 (2013), pp. 1274-1281.

5. 5) Kakami, A. and Tachibana, T.: Measurement of Thrust with Wide-Frequency Range Variation by Applying Active Control and Disturbance Observer, Aerospace Tech. Japan, 60 (2012), pp. 203-211 (in Japanese).