NUMERICAL SIMULATIONS OF OBLIQUE DETONATIONS IN SUPERSONIC COMBUSTION-CHAMBERS

被引：16

作者：

CAMBIER, JL ^{[1
]}

ADELMAN, HG ^{[1
]}

MENEES, GP ^{[1
]}

机构：

[1] NASA,AMES RES CTR,AEROTHERMODYNAM BRANCH,MOFFETT FIELD,CA 94035

来源：

关键词：

D O I：

10.2514/3.23180

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：482 / 491

页数：10

共 36 条

[11] ORAN E, 1982, COMBUST FLAME, V48, P161
[12] ORAN E, 1978, 17TH P INT S COMB, P43
[13] ORAN E, 1981, PROGR ENERGY COMBUST, V17, P1
[14] Oran E.S., 2001, NUMERICAL SIMULATION, V2nd ed.
[15] WEAK AND STRONG IGNITION .2. SENSITIVITY OF THE HYDROGEN-OXYGEN SYSTEM
ORAN, ES
BORIS, JP
[J]. COMBUSTION AND FLAME, 1982, 48 (02) : 149 - 161
[16] WEAK AND STRONG IGNITION .1. NUMERICAL SIMULATIONS OF SHOCK-TUBE EXPERIMENTS
ORAN, ES
YOUNG, TR
BORIS, JP
COHEN, A
[J]. COMBUSTION AND FLAME, 1982, 48 (02) : 135 - 148
[17] ORAN ES, 1981, P 18 S INT COMB COMB, P1641
[18] PULLIAM TH, 1986, SOLUTION METHODS COM
[19] PARALLEL COMPUTATION OF UNSTEADY, 3-DIMENSIONAL, CHEMICALLY REACTING, NONEQUILIBRIUM-FLOW USING A TIME-SPLIT FINITE-VOLUME METHOD ON ILLIAC-IV
REINHARDT, WA
[J]. JOURNAL OF PHYSICAL CHEMISTRY, 1977, 81 (25) : 2427 - 2435
[20] RHODES RP, 1962, TR AEDCTNTDR6278