CALCULATION METHOD FOR 3-DIMENSIONAL ROTATIONALLY SYMMETRICAL LAMINAR BOUNDARY LAYERS WITH ARBITRARY FREE-STREAM VELOCITY AND ARBITRARY WALL-TEMPERATURE VARIATION

被引：9

作者：

DRAKE, RM

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1953年 / 20卷 / 05期

关键词：

D O I：

10.2514/8.2633

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：309 / &

共 14 条

[1] DRAKE RM, 1952, 417 U CAL I ENG RES
[2] ECKERT E, 1942, VDI416 FORSCH
[3] ECKERT E, 1942, LUFTFAHRTFORSCHUNG, V19
[4] FROSSLING N, 1940, LUNDS U ARSSKR, V35
[5] HANDZSCHE W, 1941, JB DTSCH LUFTFAHRT 1, V76
[6] Hartree DR, 1937, P CAMB PHILOS SOC, V33, P223
[7] HOMANN F, 1936, ZAMM, V16
[8] HEAT TRANSFER TO CONSTANT-PROPERTY LAMINAR BOUNDARY-LAYER FLOWS WITH POWER-FUNCTION FREE-STREAM VELOCITY AND WALL-TEMPERATURE VARIATION
LEVY, S
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (05): : 341 - 348
[9] MANGLER W, 1948, ZAMM, V28
[10] MILLIKAN CB, 1932, T ASME, V54