Analysis of Potential Usage for Heat of Scramjet Wall

Tuijin Jishu/Journal of Propulsion Technology

Volumn 38, Issue 2, 2017, Pages 275-280

  Li, Xin Chun ^a   Wang, Zhong Wei ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

Exergy; Fuel; Heat balance; Potential working; Scramjet

Indexed keywords

COOLANTS; ENERGY CONVERSION; EXERGY; FLOW RATE; FUELING; HEAT FLUX;

COOLANT FLOW RATES; COOLING PROCESS; HEAT BALANCE; MAXIMUM TEMPERATURE; POTENTIAL WORKING; SCRAMJET; WALL HEAT FLUX; WALL TEMPERATURES;

FUELS;

EID: 85019352840     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: 10.13675/j.cnki.tjjs.2017.02.005     Document Type: Article

References (10)

1. John J B, Russell M C. Fifty Years of Hypersonic: Where We've Been, Where We've Going[J]. Progress in Aerospace Science, 2003, 39: 511-536.
2. Yu Feng, Jiang Qin, Wen Bao, et al. Numerical Analysis of Convective Heat Transfer Characteristics of Supercritical Hydrocarbon Fuel in Cooling Panel with Local Flow Blockage Structure[J]. Journal of Supercritical Fluids, 2014, 88: 8-16.
3. YANG Yang, ZHANG Lei, ZHANG Ruo-ling, et al. Design Research of an Actively Fuel-Cooled Scramjet Combustor[J]. Journal of Propulsion Technology, 2014, 35(2): 208-212.
4. WANG Xin-zhu, ZHANG Tai-chang, LU Yang, et al. An Iterative Analysis and Design Method for Study of Coupling Processes of Combustion and Heat Transfer in Actively-Cooled Scramjet Combustor[J]. Journal of Propulsion Technology, 2014, 35(2): 213-218.
5. Wen Bao, Xianling Li, Jiang Qin, et al. Efficient Utilization of Heat Sink of Hydrocarbon Fuel for Regeneratively Cooled Scramjet[J]. Applied Thermal Engineering, 2013, 33-34: 208-218.
6. Wen Bao, Jiang Qin, Weixing Zhou, et al. Parametric Performance Analysis of Multiple Re-Cooled Cycle for Hydrogen Fueled Scramjet[J]. International Journal of Hydrogen Energy, 2009, 34: 7334-7341.
7. Wen Bao, Jiang Qin, Weixing Zhou, et al. Performance Limit Analysis of Recooled Cycle for Regenerative Cooling Systems[J]. Energy Conversion and Management, 2009, 50: 1908-1914.
8. Jiang Qin, Wen Bao, Weixing Zhou, et al. Thermal Management System Performance Analysis of Hypersonic Vehicle Based on Closed Brayton Cycle[R]. AIAA 2008-5178.
9. Jiang Qin, Weixing Zhou, Wen Bao, et al. Thermodynamic Analysis and Parametric Study of a Closed Brayton Cycle Thermal Management System for Scramjet[J]. International Journal of Hydrogen Energy, 2010, 35: 356-364.
10. Aiichiro Tsukahara, Hiroyuki Yamao, Kazuyuki Miho. Advanced Thermal Protection Systems for Reusable Launch Vehicles[C]. Japan: 10th International Space Planes and Hypersonic Systems and Technologies Conference, 2001.