THE SUPERSONIC AND LOW-SPEED FLOWS PAST CIRCULAR CYLINDERS OF FINITE LENGTH SUPPORTED AT ONE END

被引：11

作者：

SYKES, DM

机构：

来源：

关键词：

D O I：

10.1017/S0022112062000270

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：367 / &

共 14 条

[1]

Goldstein Sydney, 1938, MODERN DEV FLUID DYN, V2

[2]

GOWEN FE, 1953, NACA TN2960

[3]

GREGORY N, 1950, 13436 AER RES COUN L

[4]

KIM CS, 1956, J PHYS SOC JPN, V11, P439

[5]

KONDO J, 1957, 7TH P JAP NAT CONG A, P167

LIVESEY, JL .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (10) :949-955

[7]

MCKINNEY LW, 1960, NASA TN D540

[8]

Pankhurst R.C., 1952, WIND TUNNEL TECHNIQU

[9]

POLHAMUS EC, 1959, NASA TR R29

[10] THE SUPERSONIC FLOW PAST A LEADING EDGE SEPARATION BUBBLE [J].

SHARP, AW .