A TOLERANT WIND-TUNNEL FOR INDUSTRIAL AERODYNAMICS

被引：11
作者：
PARKINSON, GV
机构：
来源：
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS | 1984年 / 16卷 / 2-3期
关键词：
D O I：
10.1016/0167-6105(84)90012-6
中图分类号：
TU [建筑科学];
学科分类号：
0813 ;
摘要：
引用
收藏
页码：293 / 300
页数：8
相关论文
共 50 条
[11]   Wind-tunnel aerodynamics in rotary tests of combat aircraft models [J].
Inst for Aerospace Research, Ottawa, Canada .
J Aircr, 4 (521-527)
[12]   Heat transfer effects on aerodynamics and implications for wind-tunnel tests [J].
Mabey, D.G. .
Journal of Aircraft, 1992, 29 (02) :224-230
[13]   Wind-tunnel aerodynamics in rotary tests of combat aircraft models [J].
Ericsson, LE ;
Beyers, ME .
JOURNAL OF AIRCRAFT, 1998, 35 (04) :521-528
[14]   A RESIDUAL BOUNDARY CORRECTION THEORY FOR THE TOLERANT WIND-TUNNEL [J].
PARKINSON, GV .
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1986, 22 (2-3) :177-184
[15]   ON PARKINSONS TOLERANT WIND-TUNNEL FOR CIRCULAR-CYLINDERS [J].
ZDRAVKOVICH, MM .
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1992, 40 (01) :71-74
[16]   CONFIGURATION CRITERIA FOR A BLOCKAGE-TOLERANT WIND-TUNNEL [J].
PARKINSON, GV ;
KONG, L ;
COOK, NJ .
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1992, 40 (02) :215-219
[17]   Sheared wing-tip aerodynamics: Wind-tunnel and computational investigation [J].
Vijgen, P.M.H.W., 1600, (26)
[18]   The modification of wind-tunnel results by the wind-tunnel dimensions [J].
Munk, MM .
JOURNAL OF THE FRANKLIN INSTITUTE, 1923, 196 :203-213
[19]   EFFECT OF WIND-TUNNEL ACOUSTIC MODES ON LINEAR OSCILLATING CASCADE AERODYNAMICS [J].
BUFFUM, DH ;
FLEETER, S .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1994, 116 (03) :513-524
[20]   SHEARED WING-TIP AERODYNAMICS - WIND-TUNNEL AND COMPUTATIONAL INVESTIGATION [J].
VIJGEN, PMHW ;
VANDAM, CP ;
HOLMES, BJ .
JOURNAL OF AIRCRAFT, 1989, 26 (03) :207-213
12345