A WING-BODY PROBLEM IN A SUPERSONIC CONICAL FLOW

被引：6

作者：

BROWNE, SH

FRIEDMAN, L

HODES, I

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1948年 / 15卷 / 08期

关键词：

D O I：

10.2514/8.11620

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：443 / 452

页数：10

共 9 条

[1] BUSEMANN A, 1942, DAL 1204, P455
[2] LINEARIZED SUPERSONIC FLOWS WITH AXIAL SYMMETRY
HAYES, WD
[J]. QUARTERLY OF APPLIED MATHEMATICS, 1946, 4 (03) : 255 - 261
[3] HAYES WD, 1946, LINEARIZED CONICAL S
[4] HAYES WD, 1947, LINEARIZED SUPERSONI
[5] JONES RT, NACA TN, V1032
[6] THE LIFT OF A DELTA-WING AT SUPERSONIC SPEEDS
STEWART, HJ
[J]. QUARTERLY OF APPLIED MATHEMATICS, 1946, 4 (03) : 246 - 254
[7] Tsien H.-S., 1938, J AERONAUT SCI, V5, P480
[8] von Karman T., 1932, T AM MATH SOC MECH E, V54, P303
[9] [No title captured]