3-DIMENSIONAL COMPRESSIBLE TURBULENT BOUNDARY-LAYER ON A SHARP CONE AT INCIDENCE IN SUPERSONIC-FLOW

被引：7

作者：

ADAMS, JC ^{[1
]}

机构：

[1] ARO INC,ARNOLD ENGN DEV CTR,VON KARMAN GAS DYNAM FACILITY,ARNOLD AF STN,TN 37389

来源：

关键词：

D O I：

10.1016/0017-9310(74)90006-4

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

引用

页码：581 / 593

页数：13

共 31 条

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[2]

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[3]

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[4]

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[5] LAMINAR BOUNDARY LAYER ON A CONE AT INCIDENCE IN SUPERSONIC FLOW [J].

BOERICKE, RR .

BRADLEY, RG .

[7] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS [J].

BRADSHAW, P .

[8]

BRAUN WH, 1959, R7 TR NASA

[9]

COOKE JC, 1961, CP635 AER RES COUNC

COOPER, P .