INVESTIGATION OF THE STARTING PROCESS OF A SUPERSONIC WIND-TUNNEL

被引：7

作者：

MATSUO, K

SASAGUCHI, K

MOCHIZUKI, H

TAKECHI, N

机构：

[1] KUMAMOTO UNIV,FAC ENGN,KUMAMOTO 860,JAPAN

[2] MITSUBISHI MOTORS CO,LTD,NAGOYA,JAPAN

来源：

BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS | 1980年 / 23卷 / 186期

关键词：

D O I：

10.1299/jsme1958.23.1975

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：1975 / 1981

页数：7

共 11 条

[1]

ANDERSON JD, 1976, GASDYNAMIC LASERS, P160

[2]

HIRAKI I, 1961, TM1 NAT AER LAB TECH

[3]

IKUI T, 1974, B JSME, V17, P731, DOI 10.1299/jsme1958.17.731

[4]

IWASAKI M, 1967, 26 KYUSH U RES I APP, P169

[5]

LIEPMANN HW, ELEMENTS GASDYNAMICS, P131

[6] HIGH-EFFICIENCY SUPERSONIC DIFFUSERS [J].

NEUMANN, EP ;

LUSTWERK, F .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (06) :369-374

[7]

NEUMANN EP, 1949, J APPL MECH-T ASME, V16, P195

[8]

Tamaki T., 1970, Bulletin of the Japan Society of Mechanical Engineers, V13, P51, DOI 10.1299/jsme1958.13.51

[9]

Tamaki T., 1971, B JSME, V14, P807, DOI DOI 10.1299/JSME1958.14.807

[10]

TUCKER ML, 1951, TN2337 NACA