CALCULATION OF 3-DIMENSIONAL SUPERSONIC-FLOW IN AN AXIAL COMPRESSOR BY A METHOD OF CHARACTERISTICS

被引：0

|

作者：

MARTINON, J

机构：

来源：

RECHERCHE AEROSPATIALE | 1978年 / 04期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：161 / 174

页数：14

相关论文

共 50 条

[21] A 3-DIMENSIONAL THEORY OF AXIAL COMPRESSOR BLADE ROWS - APPLICATION IN SUBSONIC AND SUPERSONIC FLOWS
MCCUNE, JE
JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (09): : 544 - 560
[22] 3-DIMENSIONAL FLOW IN DEEP ROTATING STALL CELLS OF AN AXIAL COMPRESSOR
MATHIOUDAKIS, K
BREUGELMANS, FAE
JOURNAL OF PROPULSION AND POWER, 1988, 4 (03) : 263 - 269
[23] MEASUREMENT OF 3-DIMENSIONAL FLOW FIELD BEHIND AN AXIAL COMPRESSOR STAGE
HIRSCH, C
KOOL, P
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1977, 99 (02): : 168 - 180
[24] METHOD OF CHARACTERISTICS FOR SUPERSONIC-FLOW OF A GUIDING CENTER PLASMA
WHANG, YC
JOURNAL OF PLASMA PHYSICS, 1972, 7 (FEB) : 87 - &
[25] ON CALCULATION OF UNSTEADY NONLINEAR 3-DIMENSIONAL SUPERSONIC FLOW PAST WINGS
KACPRZYN.JJ
ASHLEY, H
SANKARAN.R
MECHANICAL ENGINEERING, 1968, 90 (08) : 52 - &
[26] ON CALCULATION OF UNSTEADY NONLINEAR 3-DIMENSIONAL SUPERSONIC FLOW PAST WINGS
KACPRZYN.JJ
ASHLEY, H
SANKARAN.R
JOURNAL OF BASIC ENGINEERING, 1968, 90 (04): : 581 - &
[27] 3-DIMENSIONAL COMPRESSIBLE TURBULENT BOUNDARY-LAYER ON A SHARP CONE AT INCIDENCE IN SUPERSONIC-FLOW
ADAMS, JC
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1974, 17 (05) : 581 - 593
[28] THE 3-DIMENSIONAL REPRESENTATION OF THE LIFT AND PITCHING MOMENT COEFFICIENTS ON WEDGED RECTANGULAR WINGS IN SUPERSONIC-FLOW
NASTASE, A
JAKOBS, R
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1993, 73 (06): : T607 - T611
[29] MEASUREMENT OF THE 3-DIMENSIONAL TIP REGION FLOW-FIELD IN AN AXIAL COMPRESSOR
STAUTER, RC
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (03): : 468 - 476
[30] LINEARIZED CHARACTERISTICS METHOD FOR SUPERSONIC-FLOW PAST VIBRATING SHELLS
PLATZER, MF
BRIX, CW
WEBSTER, KA
AIAA JOURNAL, 1973, 11 (09) : 1302 - 1305

← 1 2 3 4 5 →