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FURTHER EXPERIMENTS ON SHOCK-TUBE WALL BOUNDARY-LAYER-TRANSITION - REPLY
被引:0
作者
:
COOK, WJ
论文数:
0
引用数:
0
h-index:
0
机构:
SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
COOK, WJ
[
1
]
CHANEY, MJ
论文数:
0
引用数:
0
h-index:
0
机构:
SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
CHANEY, MJ
[
1
]
机构
:
[1]
SVERDRUP TECHNOL INC, ARNOLD AFB, TN USA
来源
:
AIAA JOURNAL
|
1985年
/ 23卷
/ 08期
关键词
:
D O I
:
10.2514/3.8198
中图分类号
:
V [航空、航天];
学科分类号
:
08 ;
0825 ;
摘要
:
引用
收藏
页码:1298 / 1299
页数:2
相关论文
共 3 条
[1]
FURTHER EXPERIMENTS ON SHOCK-TUBE WALL BOUNDARY-LAYER-TRANSITION
[J].
CHANEY, MJ
论文数:
0
引用数:
0
h-index:
0
机构:
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
CHANEY, MJ
;
COOK, WJ
论文数:
0
引用数:
0
h-index:
0
机构:
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
COOK, WJ
.
AIAA JOURNAL,
1983,
21
(07)
:1046
-1048
[2]
CHANEY MJ, 1977, THESIS IOWA STATE U
[3]
TURBULENT SPOTS AND WALL ROUGHNESS EFFECTS IN SHOCK TUBE BOUNDARY LAYER TRANSITION
[J].
THOMPSON, WP
论文数:
0
引用数:
0
h-index:
0
THOMPSON, WP
;
EMRICH, RJ
论文数:
0
引用数:
0
h-index:
0
EMRICH, RJ
.
PHYSICS OF FLUIDS,
1967,
10
(01)
:17
-&
←
1
→
共 3 条
[1]
FURTHER EXPERIMENTS ON SHOCK-TUBE WALL BOUNDARY-LAYER-TRANSITION
[J].
CHANEY, MJ
论文数:
0
引用数:
0
h-index:
0
机构:
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
CHANEY, MJ
;
COOK, WJ
论文数:
0
引用数:
0
h-index:
0
机构:
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
IOWA STATE UNIV SCI & TECHNOL,DEPT MECH ENGN,AMES,IA 50011
COOK, WJ
.
AIAA JOURNAL,
1983,
21
(07)
:1046
-1048
[2]
CHANEY MJ, 1977, THESIS IOWA STATE U
[3]
TURBULENT SPOTS AND WALL ROUGHNESS EFFECTS IN SHOCK TUBE BOUNDARY LAYER TRANSITION
[J].
THOMPSON, WP
论文数:
0
引用数:
0
h-index:
0
THOMPSON, WP
;
EMRICH, RJ
论文数:
0
引用数:
0
h-index:
0
EMRICH, RJ
.
PHYSICS OF FLUIDS,
1967,
10
(01)
:17
-&
←
1
→