AN EXPERIMENTAL INVESTIGATION OF LEADING EDGE SHOCK-WAVE - BOUNDARY-LAYER INTERACTION AT MACH 5.8

被引：33

作者：

KENDALL, JM

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 01期

关键词：

D O I：

10.2514/8.3763

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：47 / 56

页数：10

共 18 条

[1] BALDWIN LC, 1955, GALCIT MEMORANDUM, V28
[2] BALOGA PE, 1955, GALCIT MEMORANDUM, V29
[3] VISCOUS AND LEADING-EDGE THICKNESS EFFECTS ON THE PRESSURES ON THE SURFACE OF A FLAT PLATE IN HYPERSONIC FLOW
BERTRAM, MH
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (06): : 430 - 431
[4] BERTRAM MH, 1953, NACA TN2773
[5] COHEN CB, 1955, NACA TN3326
[6] EGGERS AJ, 1952, NACA TN2646
[7] EIMER M, 1953, GALCIT MEMORANDUM, V16
[8] HAMMITT AG, 1954, WADC54257 TECHN REP
[9] HAMMITT AG, 1955, AERONAUTICAL ENG LAB, V326
[10] VISCOUS FLOW ALONG A FLAT PLATE MOVING AT HIGH SUPERSONIC SPEEDS
KUO, YH
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (02): : 125 - 136