2-DIMENSIONAL OSCILLATING AIRFOIL IN A WIND TUNNEL IN SUBSONIC FLOW

被引：23

|

作者：

BLAND, SR

机构：

来源：

SIAM JOURNAL ON APPLIED MATHEMATICS | 1970年 / 18卷 / 04期

关键词：

D O I：

10.1137/0118076

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

引用

收藏

页码：830 / +

页数：1

相关论文

共 50 条

[21] A 2ND-ORDER SOLUTION FOR AN OSCILLATING 2-DIMENSIONAL SUPERSONIC AIRFOIL
WYLLY, A
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (10): : 685 - &
[22] NEW COMPRESSIBILITY CORRECTION FOR 2-DIMENSIONAL SUBSONIC FLOW
LAITONE, EV
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (05): : 350 - 350
[23] QUASI-STEADY DERIVATIVES FOR THE SUBSONIC FLOW PAST AN OSCILLATING AEROFOIL IN A POROUS WIND TUNNEL
DRAKE, DG
[J]. AERONAUTICAL QUARTERLY, 1959, 10 (03): : 211 - 229
[24] Feasibility of airfoil tests with a samll high subsonic cryogenic wind tunnel
Yamaguchi, Y
Kashitani, M
Kaibara, K
Saito, T
[J]. ICIASF'99: INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, RECORD, 1999, : 341 - 3410
[25] Generalized vortex lattice method for oscillating thin airfoil in subsonic flow
[J]. Soviero, Paulo A.O., 1600, (31):
[26] LEADING AND TRAILING EDGE SOLUTIONS FOR THE OSCILLATING AIRFOIL IN SUBSONIC COMPRESSIBLE FLOW
KARP, SN
[J]. BULLETIN OF THE AMERICAN MATHEMATICAL SOCIETY, 1950, 56 (02) : 173 - 173
[27] A NOTE ON A SOLUTION TO POSSIO INTEGRAL EQUATION FOR AN OSCILLATING AIRFOIL IN SUBSONIC FLOW
MILES, JW
[J]. QUARTERLY OF APPLIED MATHEMATICS, 1949, 7 (02) : 213 - 216
[28] GENERALIZED VORTEX LATTICE METHOD FOR OSCILLATING THIN AIRFOIL IN SUBSONIC FLOW
SOVIERO, PAO
[J]. AIAA JOURNAL, 1993, 31 (12) : 2380 - 2382
[29] ON THE FLOW AT THE REAR OF A 2-DIMENSIONAL SUPERSONIC AIRFOIL WITH THICKNESS
PROBSTEIN, RF
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (08): : 580 - 581
[30] NUMERICAL SOLUTION OF SUBSONIC COMPRESSIBLE FLOW AT 2-DIMENSIONAL INLETS
HOWELL, RH
SPONG, ED
[J]. AIAA JOURNAL, 1969, 7 (07) : 1392 - &

← 1 2 3 4 5 →