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

[1] FLIGHT SIMULATION EQUIPMENT OF AERONAUTICAL INSTITUTE OF TECHNICAL-UNIVERSITY-DARMSTADT
HECHLER, B
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1975, 23 (10): : 368 - 371
[2] CONVERSION OF A LOW-SPEED WIND-TUNNEL TO A SNOWDRIFT WIND-TUNNEL
ANNO, Y
HOSHIBA, S
AIHARA, H
COLD REGIONS SCIENCE AND TECHNOLOGY, 1986, 12 (03) : 291 - 294
[3] GERMAN DUTCH LOW-SPEED WIND-TUNNEL DNW
SEIDEL, M
JAARSMA, F
AERONAUTICAL JOURNAL, 1978, 82 (808): : 167 - 173
[4] DESIGN OF A LOW-SPEED AXISYMMETRICAL WIND-TUNNEL CONTRACTION
ALBAYRAK, K
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1991, 37 (01) : 79 - 86
[5] LOW-SPEED WIND-TUNNEL FOR STUDYING NATURAL VENTILATION IN BUILDINGS
CHAND, I
INDIAN JOURNAL OF TECHNOLOGY, 1973, 11 (06): : 267 - 271
[6] RECENT TRENDS IN LOW-SPEED WIND-TUNNEL DESIGN AND TECHNIQUES
TEMPLIN, RJ
ANNALS OF THE NEW YORK ACADEMY OF SCIENCES, 1968, 154 (A2) : 1055 - &
[7] A FLOW VISUALIZATION TECHNIQUE FOR LOW-SPEED WIND-TUNNEL STUDIES
BIENKIEWICZ, B
CERMAK, JE
EXPERIMENTS IN FLUIDS, 1987, 5 (03) : 212 - 214
[8] DYNAMIC STABILITY DERIVATIVES EVALUATION IN A LOW-SPEED WIND-TUNNEL
GUGLIERI, G
QUAGLIOTTI, FB
JOURNAL OF AIRCRAFT, 1993, 30 (03): : 421 - 423
[9] Thermographic Transition Detection for Low-Speed Wind-Tunnel Experiments
Grawunder, M.
Ress, R.
Breitsamter, C.
AIAA JOURNAL, 2016, 54 (06) : 2012 - 2016
[10] MULTICOMPUTER INSTRUMENTATION SYSTEM FOR A NEW PRESSURIZED LOW-SPEED WIND-TUNNEL
NORTH, RJ
PARTRIDG.DW
BROWN, EC
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1973, AES9 (05) : 824 - 824

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