HIGHER-ORDER EFFECTS IN BOUNDARY-LAYER PREMIXED COMBUSTION

被引:3
作者
TREVINO, C [1 ]
STUTTGEN, W [1 ]
PETERS, N [1 ]
机构
[1] INST TECH MECH,AACHEN,GERMANY
关键词
D O I
10.2514/3.25425
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Higher-order effects in the boundary-layer theory are included in the present analysis to evaluate the interaction of the expansion process from the premixed combustion of reacting gases with the potential flowTwo cases are considered: 1) the premixed combustion process, which takes place above the flat plate, and 2) the premixed flame, which is generated in the wake of the flat plate. In both cases, the strong expansion process, when interacting with the outer inviscid flow, produces relatively strong pressure gradients, modifying the aerodynamic structure of the flow. © 1988 American Institute of Aeronautics and Astronautics.
引用
收藏
页码:237 / 242
页数:6
相关论文
共 14 条
[1]  
Goldstein S, 1933, P R SOC LOND A-CONTA, V142, P545, DOI 10.1098/rspa.1933.0187
[2]  
Hirano T, 1973, 14 S INT COMB COMB I, V14, P391, DOI [10.1016/S0082-0784(73)80038-4, DOI 10.1016/S0082-0784(73)80038-4]
[3]  
IMAI I, 1957, J AERONAUT SCI, V24, P155
[4]   ON THE FLOW OF AN INCOMPRESSIBLE VISCOUS FLUID PAST A FLAT PLATE AT MODERATE REYNOLDS NUMBERS [J].
KUO, YH .
JOURNAL OF MATHEMATICS AND PHYSICS, 1953, 32 (2-3) :83-101
[5]   A NEW APPROACH TO THIN AEROFOIL THEORY [J].
LIGHTHILL, MJ .
AERONAUTICAL QUARTERLY, 1951, 3 (03) :193-210
[6]   BOUNDARY-LAYER FLOW NEAR TRAILING EDGE OF A FLAT PLATE [J].
MESSITER, AF .
SIAM JOURNAL ON APPLIED MATHEMATICS, 1970, 18 (01) :241-&
[7]  
MESSITER AF, 1976, Z FUER ANGEWANDTE MA, V27, P634
[8]  
Sharma O. P., 1970, COMBUST SCI TECHNOL, V1, P481, DOI [10.1080/00102206908952228, DOI 10.1080/00102206908952228]
[9]  
STEWARDSON K, 1969, MATHEMATIKA, V16, P146
[10]  
Toong T.Y., 1957, 6 S COMB, P532