LOW-SPEED WIND-TUNNEL (DIAMETER 3 M) OF AERONAUTICAL INSTITUTE OF TECHNICAL-UNIVERSITY-DARMSTADT

被引：0

作者：

RETTIG, K ^{[1
]}

机构：

[1] TH DARMSTADT,INST FLUGTECH,DARMSTADT,FED REP GER

来源：

ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN | 1975年 / 23卷 / 10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

页码：364 / 366

页数：3

共 38 条

[21] LOW-SPEED AIR TUNNEL OF INSTITUTE-OF-HYDROMECHANICS AT UNIVERSITY-OF-KARLSRUHE
ERMSHAUS, R
NAUDASCHER, E
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1977, 1 (06): : 419 - 425
[22] INVESTIGATIONS INTO THE EFFECTS OF SCALE AND COMPRESSIBILITY ON LIFT AND DRAG IN THE RAE 5M PRESSURISED LOW-SPEED WIND-TUNNEL
FIDDES, SP
KIRBY, DA
WOODWARD, DS
PECKHAM, DH
AERONAUTICAL JOURNAL, 1985, 89 (883): : 93 - 108
[23] WIND-TUNNEL INTERFERENCE ON UNSTEADY TWO-DIMENSIONAL AEROFOIL MOTIONS IN LOW-SPEED FLOWS
CHEUNG, CW
HANCOCK, GJ
AERONAUTICAL JOURNAL, 1988, 92 (913): : 115 - 121
[24] MIXED CONVECTION FROM A ROTATING HORIZONTAL HEATED CYLINDER PLACED IN A LOW-SPEED WIND-TUNNEL
JONES, J
POULIKAKOS, D
OROZCO, J
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 1988, 9 (02) : 165 - 173
[25] LOW-SPEED AERODYNAMIC TESTING OF VTOL MODELS - METHOD FOR COMPENSATION OF WIND-TUNNEL INTERFERENCE EFFECTS
SCHAUB, UW
BASSETT, RW
CANADIAN AERONAUTICS AND SPACE JOURNAL, 1971, 17 (06): : 245 - &
[26] THE MINITUFT SURFACE FLOW VISUALIZATION METHOD - EXPERIENCE OF USE IN THE RAE 5M PRESSURIZED LOW-SPEED WIND-TUNNEL
DOBNEY, DG
HANSON, P
FIDDES, SP
AERONAUTICAL JOURNAL, 1986, 90 (891): : 10 - 17
[27] UNSTEADY PRESSURE MEASUREMENTS IN A LOW-SPEED WIND-TUNNEL USING A LARGE SIGNAL-TO-NOISE TECHNIQUE
NAGIB, HM
CORKE, TC
BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1976, 21 (10): : 1237 - 1237
[28] WIND-TUNNEL RESULTS FOR A MODIFIED 17-PERCENT-THICK LOW-SPEED AIRFOIL SECTION.
McGhee, Robert J.
Beasley, William D.
NASA Technical Paper, 1981,
[29] SOME CHARACTERISTICS OF LONGITUDINAL VORTICES PRODUCED BY LINE-SOURCE HEATING IN A LOW-SPEED WIND-TUNNEL
SMITH, MC
HAINES, DA
MAIN, WA
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1986, 29 (01) : 59 - 68
[30] SOME LOW-SPEED WIND-TUNNEL TECHNIQUES FOR MEASUREMENT OF OSCILLATORY AERODYNAMIC DERIVATIVES ON JET-BLOWING MODELS
OWEN, TB
JOURNAL OF SOUND AND VIBRATION, 1966, 4 (03) : 507 - &

← 1 2 3 4 →