Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6234088B2 - - Google Patents
[go: Go Back, main page]

JPS6234088B2 - - Google Patents

Info

Publication number
JPS6234088B2
JPS6234088B2 JP18342681A JP18342681A JPS6234088B2 JP S6234088 B2 JPS6234088 B2 JP S6234088B2 JP 18342681 A JP18342681 A JP 18342681A JP 18342681 A JP18342681 A JP 18342681A JP S6234088 B2 JPS6234088 B2 JP S6234088B2
Authority
JP
Japan
Prior art keywords
wind
section
flow
wind tunnel
opening
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP18342681A
Other languages
Japanese (ja)
Other versions
JPS5885131A (en
Inventor
Hideki Maeda
Yasuo Ide
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP18342681A priority Critical patent/JPS5885131A/en
Publication of JPS5885131A publication Critical patent/JPS5885131A/en
Publication of JPS6234088B2 publication Critical patent/JPS6234088B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06Measuring arrangements specially adapted for aerodynamic testing

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

【発明の詳細な説明】 本発明は風洞、特に胴内に微風流速を発生させ
る風洞に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a wind tunnel, and more particularly to a wind tunnel that generates a breeze velocity within a shell.

超高層ビルの建設に伴なう風害、煙突やトンネ
ル排気筒から排出される有害ガスや熱による公
害、その他、害に限らず風の作用によつて生じる
様々な影響を実験室内で模擬する場合には風洞が
用いられている。
When simulating in a laboratory the effects of wind damage caused by the construction of skyscrapers, pollution caused by harmful gases and heat emitted from chimneys and tunnel exhaust stacks, and other effects not limited to harm caused by the action of wind. A wind tunnel is used.

第1図には煙の拡散状況を観察する場合の吹出
し式風洞が示されている。
Figure 1 shows a blow-out type wind tunnel for observing the state of smoke diffusion.

風洞は連続し、かつ種々に形の異なる胴から形
成されており、胴の一端に配設された送風機01
で発生された風の流れは導風部02で拡大され格
子などの整流装置04が胴内に配置された整流部
03および胴の断面積が急激に小さくなる縮流部
05で均一な流れに整流される。
The wind tunnel is continuous and is formed from a variety of differently shaped shells, and a blower 01 is installed at one end of the shell.
The flow of wind generated in the air is expanded in the wind guiding part 02, and is made into a uniform flow in the rectifying part 03 where a rectifying device 04 such as a grid is placed inside the body, and in the contracting part 05 where the cross-sectional area of the body rapidly decreases. rectified.

この均一に整流された流れは必要に応じて乱流
発生装置06で適度に乱されて測定部07に入り
最後に排出口09から胴外に排出される。
This uniformly rectified flow is appropriately disturbed by a turbulence generating device 06 as required, enters a measuring section 07, and is finally discharged to the outside of the body through a discharge port 09.

上記測定部07内には模型08が配設され模型
08から煙などのトレーサーガス010を吐出し
その拡散状況を観察あるいは測定している。
A model 08 is disposed within the measurement section 07, and a tracer gas 010 such as smoke is discharged from the model 08 and its diffusion state is observed or measured.

風洞実験では、自然界における現象を実験室内
に持ち込む為、いわゆる相似則を一致させた実験
を行なわなければならない。特に模型の縮少に伴
ない、模型に当る風をそれに見合つただけ遅くし
なければならないが、たとえば模型の縮尺が百分
の1で風速5m/sを模擬しようとすると測定部
07での風速は0.5m/sである。
In wind tunnel experiments, in order to bring phenomena from the natural world into the laboratory, it is necessary to conduct experiments that match the so-called law of similarity. In particular, as the model is reduced in size, the wind hitting the model must be slowed down accordingly. For example, if the scale of the model is 1/100 and we are trying to simulate a wind speed of 5 m/s, the wind speed at measurement section 07 will be is 0.5m/s.

風洞の胴内の風速が早い場合には無視できる
様々な問題も、この様な微風速下においては大問
題となることも多い。
Various problems that can be ignored when the wind speed inside the wind tunnel is high often become major problems at such low wind speeds.

たとえば胴の温度の点であり、特に流路が拡大
する整流部03と、測定を行なう測定部07で不
都合となる。すなわち、胴の壁を伝わつて胴内に
熱が入る場合や、熱が出ていくことによつて生じ
る胴内の対流の問題であつて、風洞が直射日光の
影響を受ける場合や、地面に胴が接している様な
場合、胴の下方は冷たく、逆に上方が暑いという
アンバランスが生じると上下方向に対流が生じ、
また温度による比重の差からも上下方向の流速が
均一にならないものである。この点流路が拡大し
流速の遅くなる整流部03で乱れが生じ後流側へ
影響を与え、また測定部07ではその乱れ自身が
測定結果を左右することになつてしまう。
For example, this is a problem in terms of the temperature of the body, and is particularly inconvenient in the rectifying section 03 where the flow path expands and in the measuring section 07 that performs measurements. In other words, it is a problem of convection inside the shell that occurs when heat enters the shell through the walls of the shell or when heat leaves the shell, and when the wind tunnel is affected by direct sunlight or when the ground When the bodies are in contact with each other, if there is an imbalance in which the lower part of the body is cold and the upper part is hot, convection will occur in the vertical direction.
Further, due to the difference in specific gravity due to temperature, the flow velocity in the vertical direction is not uniform. In the rectifying section 03 where the flow path expands and the flow velocity slows down, turbulence occurs and affects the downstream side, and in the measuring section 07, the turbulence itself influences the measurement results.

第2図には胴の上方が下方より温度が高い場合
の縮流部05から測定部07入口にかけての流れ
概要図である。
FIG. 2 is a schematic diagram of the flow from the contraction section 05 to the inlet of the measurement section 07 when the upper part of the shell is higher in temperature than the lower part.

風の流れF1は上向きとなり測定部07上方に
片寄るため、上方の風速が速く下方が遅くなり、
縮流部05の底部には渦流012が生じることも
ある。そうすると測定部07では均一の流れを得
ることができず風速分布を持つた流れとなつてし
まう。
The wind flow F 1 is directed upward and is biased above the measurement part 07, so the wind speed is faster in the upper part and slower in the lower part.
A vortex 012 may be generated at the bottom of the contraction section 05. In this case, a uniform flow cannot be obtained in the measuring section 07, and the flow ends up having a wind speed distribution.

第3図は上記とは逆に胴の下方が上方より高温
の場合の縮流部05から測定部07入口にかけて
の流れの概要図である。
FIG. 3 is a schematic diagram of the flow from the contraction section 05 to the inlet of the measuring section 07 when, contrary to the above, the lower part of the body is hotter than the upper part.

風の流れF2は逆に下向きとなり測定部07下
方に片寄るため、上部の風速が遅く下部が速い風
速分布を持つた流れとなる。
On the contrary, the wind flow F 2 is directed downward and is biased below the measuring section 07, resulting in a flow with a wind speed distribution in which the wind speed is slow in the upper part and fast in the lower part.

以上従来ものの風洞では胴外温度差により胴自
身上・下に温度差が発生し、これの影響で測定部
07で風速分布、及び風向分布が生じ一定風速、
一定風向という風洞本来の特性を失い実験ができ
なくなる。
As described above, in the conventional wind tunnel, a temperature difference occurs between the top and bottom of the shell due to the temperature difference outside the shell, and due to this influence, wind speed distribution and wind direction distribution occur in the measurement section 07, resulting in a constant wind speed,
The wind tunnel's original characteristic of constant wind direction will be lost, making experiments impossible.

本発明はこの欠点を排除するものであつて、連
続した筒状の胴内に発生された風の流れを縮流し
て均一な流れを作る縮流部と、同縮流部と連続し
均一にされた風を導入される測定部とを有する風
洞において、上記測定部の上流端に接続されると
ともに縮流部内に上流側へ向けて拡大して開口す
る内筒を配設し、上記縮流部に開口部を設け、か
つ同開口部を通つて胴外に排出される風量を調整
する調整機構を備えたことを特徴とし、その目的
とするところは風導の胴を介しての熱の流出入に
伴なう風洞測定部における風速分布を小さくし自
然条件に極めて類似した条件において、実験を行
うことの可能な微風速風洞を提供するものであ
る。
The present invention eliminates this drawback, and includes a constriction section that constricts the flow of wind generated in a continuous cylindrical body to create a uniform flow, and a constriction section that creates a uniform flow by constricting the flow of air generated in a continuous cylindrical body. In the wind tunnel, an inner cylinder is provided which is connected to the upstream end of the measurement part and expands and opens toward the upstream side within the contraction part, It is characterized by having an opening in the body and an adjustment mechanism for adjusting the amount of air discharged outside the body through the opening. The purpose of the present invention is to provide a wind tunnel with low wind speeds that allows experiments to be conducted under conditions extremely similar to natural conditions by reducing the wind speed distribution in the wind tunnel measurement section due to inflow and outflow.

本発明は上記したように縮流部の内側に、上流
側へ向けて拡大して開口する内筒を配設し、内筒
の下流側端と測定部を接続したことが1つの特徴
である。すなわちこの内筒が適当な断面形状を有
し縮流作用を行なうことになる。
As described above, one feature of the present invention is that an inner tube that expands and opens toward the upstream side is provided inside the contraction section, and the downstream end of the inner tube is connected to the measurement section. . In other words, this inner cylinder has an appropriate cross-sectional shape and performs a flow contracting action.

一方上記縮流部に開口部を設けたことが本発明
の2つの特徴である。すなわち第2図および第3
図に示したような縮流部の上方または下方に片寄
る流速変化の大きなものや渦流は開口部を通つて
胴外に排出される。
On the other hand, two features of the present invention are that an opening is provided in the contracted flow section. That is, Figures 2 and 3
As shown in the figure, flow velocity changes that are large or vortices that are biased upward or downward at the contraction section are discharged to the outside of the shell through the opening.

更に本発明では、開口部を通つて胴外に排出さ
れる風の量を調整する調整機構を有している。
Further, the present invention includes an adjustment mechanism that adjusts the amount of air discharged outside the shell through the opening.

従つて測定部に送られる風は、内筒の先端部よ
り入る流速変化の少ない風を該内筒で縮流したも
ののみとなり、均一の流れが得られることにな
る。
Therefore, the air sent to the measuring section is only the air that enters from the tip of the inner cylinder and has a small change in velocity, and is contracted in the inner cylinder, resulting in a uniform flow.

以下本発明を第4図および第5図に示す一実施
例の風洞について説明するが、この例においても
吹出し型の風洞に適用し符号2ないし7を付した
ものは第1図で02ないし07を付したものと同
一の構造を有するので説明か省略する。
The present invention will be described below with respect to an embodiment of the wind tunnel shown in FIG. 4 and FIG. Since it has the same structure as the one with , the explanation will be omitted.

11は縮流部5を形成する胴内に配設される内
筒であつて、後流端は測定部7の内壁に接続され
ており、拡大して広がる上流端は整流部3内に配
置した整流装置4にまで達している。この内筒1
1は薄板から構成されており、その形状は縮流部
の内壁形状と略相似形状を有している。
Reference numeral 11 denotes an inner cylinder disposed within the body forming the flow contraction section 5, the trailing end of which is connected to the inner wall of the measurement section 7, and the enlarged upstream end disposed within the rectification section 3. The current reaches the rectifying device 4. This inner cylinder 1
1 is composed of a thin plate, and its shape is approximately similar to the shape of the inner wall of the contraction section.

12aおよび12bは縮流部5の上下胴壁に
夫々貫通させて設けた適当な断面積を有する開口
部である。
Reference numerals 12a and 12b are openings having an appropriate cross-sectional area, which are provided through the upper and lower body walls of the contracting portion 5, respectively.

同開口部12a・12bには夫々排気フアン1
3aおよび13bが装備されており、風洞の測定
部7内に設置された温度センサ14a・14bの
出力を受けて制御信号を出す制御器15によつて
排気フアン13a・13bの回転数は制御され
る。これら排気フアン13a・13b、温度セン
サ14a・14bおよび制御器15で調整機構が
構成される。
Exhaust fans 1 are provided in the openings 12a and 12b, respectively.
3a and 13b, and the rotational speed of the exhaust fans 13a and 13b is controlled by a controller 15 that receives the outputs of temperature sensors 14a and 14b installed in the measurement section 7 of the wind tunnel and outputs a control signal. Ru. These exhaust fans 13a and 13b, temperature sensors 14a and 14b, and controller 15 constitute an adjustment mechanism.

さて日射、あるいは周囲温度の影響等何んらか
の原因により導風管部2の上方と下方に温度差が
生じた場合内部の風の流れにも温度差が生じる。
Now, if a temperature difference occurs between the upper part and the lower part of the air guide pipe section 2 due to some cause such as sunlight or the influence of ambient temperature, a temperature difference will also occur in the internal air flow.

風の上層部の温度が高く、下層部が低い場合に
は総じて胴内の上部が加速される。(第5図点線
で示してある。) 従つて一対の温度センサ14a・14bで測定
される測定部7内の風の温度には差が生じ、上方
の温度センサ14aの出力が大きく、下方の温度
センサ14bの出力が小さくなる。
When the upper part of the wind has a high temperature and the lower part has a low temperature, the upper part of the body is generally accelerated. (It is shown by the dotted line in Figure 5.) Therefore, there is a difference in the temperature of the wind inside the measuring section 7 measured by the pair of temperature sensors 14a and 14b, and the output of the upper temperature sensor 14a is large, while the output of the lower temperature sensor 14a is large. The output of the temperature sensor 14b becomes smaller.

このような場合、上記鉛直方向の風速分布を一
定にするよう制御器15は上記温度センサ14
a・14bの出力の差を受け、排気フアン13a
の回転数を上げ前記上部を開口部12aからの排
出量を多くするとともに下部の排気フアン13b
の回転数を下げることにより下部の開口部12b
からの排出量を少なくする。これにより第5図実
験で示すようなより均一化された風速分布を得
る。
In such a case, the controller 15 controls the temperature sensor 14 so as to keep the vertical wind speed distribution constant.
In response to the difference in output between a and 14b, the exhaust fan 13a
The rotation speed of the upper part is increased to increase the amount of exhaust from the opening 12a, and the lower part of the exhaust fan 13b is
By lowering the rotation speed of the lower opening 12b.
Reduce emissions from As a result, a more uniform wind speed distribution as shown in the experiment in FIG. 5 is obtained.

なおこの場合の平均風速は図示されていない風
洞のブロワーで調整するものである。
Note that the average wind speed in this case is adjusted by a blower in a wind tunnel (not shown).

以上述べたように、本実施例の風洞縮流部5
上・下壁面に開口部12a・12bを設けかつ排
気フアン13a・13bを備えたことにより上層
もしくは下層の高温層すなわち加速域層の風と低
温層すなわち低速域層の風の流れを夫々必要な量
だけ調整して胴外に排出させるとともに縮流部5
の内側に設けた内筒11により前記開口部12
a・12bへ流出する風の流れと測定部7へ流れ
る風を安定して分離するようにしたので微風速下
で胴の上下で温度差がある場合においても一定速
度と一定風向の気流が得られる。
As described above, the wind tunnel contraction section 5 of this embodiment
By providing openings 12a and 12b on the upper and lower walls and providing exhaust fans 13a and 13b, the wind flows in the high temperature layer, that is, the acceleration region layer, and the wind in the low temperature layer, that is, the low speed region layer, respectively, as required. The volume is adjusted and discharged outside the body, and the flow contracting part 5
The opening 12 is opened by an inner cylinder 11 provided inside the opening 12.
Since the wind flowing out to a and 12b and the wind flowing to the measuring part 7 are stably separated, even when there is a temperature difference between the upper and lower parts of the body at a slight wind speed, an air flow of a constant speed and a constant wind direction can be obtained. It will be done.

なお上記実施例では縮流部5の上下壁にのみ開
口部12を設けるとともに上下にのみ2重構造と
なる内筒11を配設したが、胴の周囲全域に2重
構造となる内筒を挿入し、かつ側面にも適当な開
口部を開けるようにしてももちろん良い。
In the above embodiment, the openings 12 were provided only in the upper and lower walls of the contraction section 5, and the inner cylinders 11 having a double structure were provided only at the top and bottom, but the inner cylinders having a double structure were provided throughout the circumference of the body. Of course, it may be inserted and an appropriate opening may also be made on the side.

更に、開口部12a・12bを通る風量調整は
排気フアン13a・13bによらず、弁等によつ
て開口面積を変化させるようにしても良い。
Further, the air volume passing through the openings 12a and 12b may be adjusted by changing the opening area by using a valve or the like instead of using the exhaust fans 13a and 13b.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来の風洞の全体説明図、第2図およ
び第3図は従来の風洞内の流れを示す図、第4図
は本発明の一実施例の風洞の要部のみを示した縦
断面図、第5図は測定部入口の風速を示したグラ
フである。 3:整流部、4:整流装置、5:縮流部、7:
測定部、11:内筒、12a,12b:開口部、
13a,13b:排気フアン、14a,14b:
温度センサ、15:制御器。
Figure 1 is an overall explanatory diagram of a conventional wind tunnel, Figures 2 and 3 are diagrams showing the flow inside a conventional wind tunnel, and Figure 4 is a longitudinal section showing only the main parts of a wind tunnel according to an embodiment of the present invention. The top view and FIG. 5 are graphs showing the wind speed at the entrance of the measuring section. 3: Rectifier section, 4: Rectifier device, 5: Contraction section, 7:
Measuring part, 11: inner cylinder, 12a, 12b: opening,
13a, 13b: Exhaust fan, 14a, 14b:
Temperature sensor, 15: Controller.

Claims (1)

【特許請求の範囲】[Claims] 1 連続した筒状の胴内に発生された風の流れを
縮流して均一な流れを作る縮流部と、同縮流部と
連続し均一にされた風を導入される測定部とを有
する風洞において、上記測定部の上流端に接続さ
れるとともに縮流部内に上流側へ向けて拡大して
開口する内筒を配設し、上記縮流部に開口部を設
け、かつ同開口部を通つて胴外に排出される風量
を調整する調整機構を備えたことを特徴とする風
洞。
1. It has a constriction section that constricts the flow of wind generated in a continuous cylindrical body to create a uniform flow, and a measurement section that is continuous with the constriction section and introduces the uniform air. In the wind tunnel, an inner cylinder is provided that is connected to the upstream end of the measurement section and expands toward the upstream side in the contraction section, and an opening is provided in the contraction section, and the opening is opened in the contraction section. A wind tunnel characterized by being equipped with an adjustment mechanism that adjusts the amount of air that passes through the tunnel and is discharged outside the body.
JP18342681A 1981-11-16 1981-11-16 Wind tunnel Granted JPS5885131A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18342681A JPS5885131A (en) 1981-11-16 1981-11-16 Wind tunnel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18342681A JPS5885131A (en) 1981-11-16 1981-11-16 Wind tunnel

Publications (2)

Publication Number Publication Date
JPS5885131A JPS5885131A (en) 1983-05-21
JPS6234088B2 true JPS6234088B2 (en) 1987-07-24

Family

ID=16135562

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18342681A Granted JPS5885131A (en) 1981-11-16 1981-11-16 Wind tunnel

Country Status (1)

Country Link
JP (1) JPS5885131A (en)

Also Published As

Publication number Publication date
JPS5885131A (en) 1983-05-21

Similar Documents

Publication Publication Date Title
KR840007949A (en) Secondary air conditioner
CN105987773B (en) Retardance formula total temperature probe
JP7421769B2 (en) Duct pressure measurement structure and wind tunnel test equipment
GB2065898A (en) Air flow rate measuring device
Jiao et al. Experimental study on the effect of canyon cross wind yaw angle on airflow and flame characteristics in a tunnel
CN114878134B (en) A small forest fire combustion wind tunnel experimental platform with a variable environment combustion chamber
Zhang et al. Experimental and numerical study of the effect of perimeter jet enhancement on the capture velocity of a rectangular exhaust hood
JPS6234088B2 (en)
JPH05288384A (en) Air curtain device
JPH08182791A (en) Air inflow adjustment mechanism at the air intake of a wind tunnel device
CN115618758A (en) Electric arc heating hypersonic wind tunnel front chamber and pneumatic design method thereof
JPH0217315Y2 (en)
JPS6256454B2 (en)
US2618972A (en) Testing apparatus for scale models of aerodynamic ducts
CN117782505A (en) A hot calibration wind tunnel structure
JP2529478Y2 (en) Variable air volume unit
CN209198041U (en) A kind of direct current of band bypass blows formula gust wind tunnel
CN204389066U (en) There is the retardance formula total temperature probe of circular air intake opening
JPS61145236U (en)
CN109632248B (en) Blowing type active flow-increasing gust wind tunnel
CN223756287U (en) A heat transfer wind tunnel test bench
Gribkov et al. Modelling of the Initial Part of a Smoke Plume from a Four-Flue Stack at a Thermal Power Station
JPH08285645A (en) Double venturi type current meter
JPS64625B2 (en)
JPH0318835Y2 (en)