COMPUTATION OF STEADY NOZZLE-FLOW BY A TIME-DEPENDENT METHOD

被引：9

作者：

CLINE, MC ^{[1
]}

机构：

[1] UNIV CALIF,LOS ALAMOS SCI LAB,LOS ALAMOS,NM 87544

来源：

AIAA JOURNAL | 1974年 / 12卷 / 04期

关键词：

D O I：

10.2514/3.49263

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：419 / 420

页数：2

共 11 条

[1]

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[2]

BROWN EF, 1972, AIAA72680 PAP

[3] TRANSONIC FLOWFIELD IN A SUPERSONIC NOZZLE WITH SMALL THROAT RADIUS OF CURVATURE [J].

CUFFEL, RF ;

BACK, LH ;

MASSIER, PF .

AIAA JOURNAL, 1969, 7 (07) :1364-&

[4]

LAVAL P, 1971, LECT NOTES PHYS, V8, P187

[5]

MACCORMACK RW, 1969, AIAA69354 PAP

[6] TIME-DEPENDENT CALCULATIONS FOR TRANSONIC NOZZLE FLOW [J].

MIGDAL, D ;

KLEIN, K ;

MORETTI, G .

AIAA JOURNAL, 1969, 7 (02) :372-&

[7] ERROR MINIMIZATION TECHNIQUE WITH APPLICATION TO A TRANSONIC NOZZLE SOLUTION [J].

PROZAN, RJ ;

KOOKER, DE .

JOURNAL OF FLUID MECHANICS, 1970, 43 :269-&

[8]

SAUNDERS LM, 1966, BSVDP66TN001 CR82601

[9] DETERMINATION OF INTERNAL GAS-FLOWS BY A TRANSIENT NUMERICAL TECHNIQUE [J].

SERRA, RA .

AIAA JOURNAL, 1972, 10 (05) :603-&

[10]

THORNOCK RL, 1968, D620375 BOEING CO DO

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