Numerical Analysis of Aerospike Engine Nozzle Performance at Various Truncation Lengths

被引：0
作者：
Dakka, Sam [1 ]
Dennison, Oliver [1 ]
机构：
[1] Univ Nottingham, Nottingham, England
来源：
INTERNATIONAL JOURNAL OF AVIATION AERONAUTICS AND AEROSPACE | 2021年 / 8卷 / 02期
关键词：
CONTOUR;
D O I：
10.15394/ijaaa.2021.1601
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
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页码：1 / 23
页数：24
相关论文
共 14 条
[1]  
Ali Bani A., 2016, DESIGN ANAL AXISYMME
[2]   APPROXIMATE METHOD FOR PLUG NOZZLE DESIGN [J].
ANGELINO, G .
AIAA JOURNAL, 1964, 2 (10) :1834-1835
[3]  
ANSYS, 2009, EV GRAD DER
[4]  
ANSYS, 2009, SPAT DISCR
[5]  
Boeing, 1997, XRS 2200 LIN AER ENG
[6]  
Bravo L., 2017, DSIAC J, V4, P1
[7]   Developing Computational Fluid Dynamics (CFD) Models to Evaluate Available Energy in Exhaust Systems of Diesel Light-Duty Vehicles [J].
Fernandez-Yanez, Pablo ;
Armas, Octavio ;
Gomez, Arantzazu ;
Gil, Antonio .
APPLIED SCIENCES-BASEL, 2017, 7 (06)
[8]  
Johnson P, 2019, CFD ANAL LINEAR AERO
[9]  
Khan S. U., 2014, COMSATS SCI VIS, V20, P25
[10]  
Nazarinia M., 2005, 11 AUSTR INT AER C A
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