Experimental Investigation of Transient Flow Measurement in the Ram-Accelerator High Pressure Pneumatic System

Author:

Liu Yang1,Song Xiao Dong1,Yao Xiao Xian1,Li Kun2

Affiliation:

1. Beijing Institute of Technology

2. Aerodynamic Technology Academy of China Aerospace Science and Industry Corporation

Abstract

A high-pressure-pneumatic mass flow control test-bed using inert medium was built in order to study the transient flow characteristic of high pressure gas feed system in ram accelerator. The structure of a new type measurement system of transient flow characteristic experiments applied to the test-bed was introduced as also. Measurement tests that high pressure gas-flow ejecting into a tank with exhaust-back-pressure through a high pressure fueling valve were conducted to ascertain the transient discharge coefficient. The results suggest that: The transient discharge coefficient increases with the inlet pressure difference of high pressure fueling valve according to polynomial law. Correlations between inlet pressure difference and transient discharge coefficient was obtained based on the experimental data. The correlation coefficient between the least square fitting curve of the correlations and experimental results reaches 0.994.The system could be used to study the change regularity of pressure and time in the fueling process of high pressure gas.

Publisher

Trans Tech Publications, Ltd.

Reference4 articles.

1. J-F. Legendre, M. griraud and M. Henner : Ram-accelerator A new hypervelocity launcher for ballistic studies, International Journal of Impact Engineering 23(1999) 533-545.

2. C. Knowlen,B. Joseph A.P. Bruckner: Ram Accelerator as an Impulsive Space Launcher, International Space Development Conference, May 25-28, 2007, Dallas TX.

3. YANG Jun-rong, Mi Liang-chuan, ZHAO Hua: Feasibility Analysis of a Type of Soft Firing Technology with Pneumatic Transmission, Journal of CHINA ORDANCE, 2006, 2(4).

4. Gritsch M, S aumweber C. Effect of internal coolant crossflow orientation on the discharge coefficient of shaped film-cooling holes . ASME Journal of Turbomachinery, 2000, 122(1).

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