SHOULDER PRESSURES FOR SLENDER CONE-AFTERBODY COMBINATIONS IN HYPERSONIC FLOW

被引：1

作者：

FIORINO, TD

RASMUSSE.ML

机构：

[1] University of Oklahoma, Aerospace and Mechanical Engineering, Norman, OK

来源：

关键词：

D O I：

10.2514/3.5061

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：169 / &

共 9 条

[1]

ADAMSON D, 1961, HANDBOOK SUPERSONIC, V3

[2]

CHERNYI GG, 1961, INTRODUCTION HYPERSO, P227

[3]

CLIPPINGER RF, 1950, 729APGBRL BALL RES L

[4] ON HYPERSONIC FLOW PAST AN UNYAWED CONE [J].

RASMUSSEN, ML .

[5]

SIMS JL, 1964, SP3004 NACA

[6]

SYVERTSON CA, 1957, 1328 NACA

[7] PRESSURE DISTRIBUTION ON CONE-CYLINDERS IN HYPERSONIC FLOW [J].

TOURYAN, KJ ;

CLARK, GE ;

RIGALI, DJ .

[8]

VANDYKE MD, 1954, 1194 NACA REP

[9]

1953, NACA1135 REP