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JPS6256454B2 - - Google Patents
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JPS6256454B2 - - Google Patents

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Publication number
JPS6256454B2
JPS6256454B2 JP17601381A JP17601381A JPS6256454B2 JP S6256454 B2 JPS6256454 B2 JP S6256454B2 JP 17601381 A JP17601381 A JP 17601381A JP 17601381 A JP17601381 A JP 17601381A JP S6256454 B2 JPS6256454 B2 JP S6256454B2
Authority
JP
Japan
Prior art keywords
wind
flow
section
wind tunnel
measurement
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
JP17601381A
Other languages
Japanese (ja)
Other versions
JPS5877633A (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 JP17601381A priority Critical patent/JPS5877633A/en
Publication of JPS5877633A publication Critical patent/JPS5877633A/en
Publication of JPS6256454B2 publication Critical patent/JPS6256454B2/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、文献
(「山越え排ガス拡散現象の可視化風洞実験」日本
気象学会九州支部講演要旨集、第5号、1983年)
にも紹介されたような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. References ("Wind tunnel experiment for visualizing the phenomenon of exhaust gas diffusion over mountains" Collection of lecture abstracts of the Kyushu branch of the Japan Meteorological Society, No. 5, 1983)
A wind tunnel like the one introduced in

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 a wind speed of 5 m/s is to be simulated, the wind speed at the 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では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.
Furthermore, the flow velocity in the vertical direction is not uniform due to the difference in specific gravity due to temperature. 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
方片寄るため、上部の風速が遅く下部が速い風速
分布を接つた流れとなる。
On the contrary, the wind flow F 2 is directed downward and is biased toward the lower part of the measuring section 07, so that the flow has 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 connected to the upstream end of the measurement part and expands and opens toward the upstream side in the contraction part, and The purpose of this is to reduce the wind velocity distribution in the wind tunnel measurement area due to the flow of heat through the wind guide shell, and to create conditions that are extremely similar to natural conditions. The purpose of this project is to provide a wind tunnel with low wind speeds in which experiments can be conducted.

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.

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
のとなり、均一の流れが得られることになる。
Therefore, the wind sent to the measuring section is the wind that enters from the tip of the inner cylinder and has a small change in flow velocity, and is contracted in the inner cylinder, so that a uniform flow is obtained.

以下本発明を第4図ないし第6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たものであり、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は省略
する。
The present invention will be described below with respect to an embodiment of the wind tunnel shown in FIGS. 4 to 6. In this example, too, the present invention is applied to a blow-out type wind tunnel, and those designated by numerals 2 to 7 are shown in FIG. Since they have the same structure as those marked with 02 to 07, their 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内に設
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 located 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.

12は縮流部5の上下胴壁に貫通させて設けた
適当な断面積を有する複数の開口部である。
Reference numeral 12 designates a plurality of openings having appropriate cross-sectional areas, which are provided through the upper and lower body walls of the contracting portion 5.

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。
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.

第6図は以上の場合の流れ模様を図示したもの
であるが図中、点線で示したのが第2図で示した
と同じ従来ものの風の流れであり実線が本実施例
の風洞における風の流れを示している。また第7
図に測定室部における鉛直方向の風速分布を示し
ており第6図同様点線が従来のもので実線が本実
施例の場合である。
Figure 6 shows the flow pattern in the above case. In the figure, the dotted line is the flow of the conventional wind, which is the same as that shown in Figure 2, and the solid line is the flow of the wind in the wind tunnel of this example. It shows the flow. Also the 7th
The figure shows the wind speed distribution in the vertical direction in the measurement chamber, where the dotted line is the conventional one and the solid line is the one of this embodiment, as in FIG. 6.

第6図点線で示すように上層部に風の流れが集
まり下層部には渦流さえ生じる。このため、従来
の風洞では測定部での風速分布は第7図の点線の
如く、上層部が加速され下層部が減速された分布
形状を示している。
As shown by the dotted line in Figure 6, wind flows gather in the upper layer and even create vortices in the lower layer. Therefore, in the conventional wind tunnel, the wind speed distribution at the measuring section shows a distribution shape in which the upper layer is accelerated and the lower layer is decelerated, as shown by the dotted line in FIG.

一方、本実施例の風洞では上層部すなわち、縮
流部5入口部で縮流部5と内筒11の上流端との
間にきた高温でかつ加速された風の流れは測定部
7の方に流れるより抵抗が小さい縮流部5に開口
した開口部12へ流れ胴外に排出される。
On the other hand, in the wind tunnel of this embodiment, the flow of high-temperature and accelerated wind that comes between the upper part, that is, the inlet of the contracting part 5 and the upstream end of the inner cylinder 11, is directed toward the measuring part 7. The flow flows to the opening 12 opened in the contracted flow section 5, where the resistance is lower than that of the flow, and is discharged to the outside of the barrel.

下層部の場合、開口部12を設けたことにより
従来より流れ易くなるため上向きの流れが修正さ
れる方向となりかつ渦流が消滅する。
In the case of the lower layer, the provision of the opening 12 makes the flow easier than before, so the upward flow is corrected and the vortex disappears.

なお逆に下方の温度が上方より高い場合には上
記と逆の現象となる。
On the other hand, if the lower temperature is higher than the upper temperature, the opposite phenomenon occurs.

また開口部12から胴内の流れが排出されるた
めに従来に比べ、ブロワーの回転数を多少上げる
ことが必要であることは言うまでもない。
Furthermore, since the flow inside the cylinder is discharged from the opening 12, it goes without saying that it is necessary to increase the rotational speed of the blower somewhat compared to the conventional blower.

従つて風洞風速がたとえば0.5m/s以下の微
風速域において胴内の上・下温度差により生じて
いた風速分布は、本実施例の風洞のように縮流部
5上・下壁面に適当断面積を有し適当数の開口部
12を設ける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
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。
Therefore, the wind speed distribution that was caused by the temperature difference between the top and bottom inside the shell in a slight wind speed region where the wind tunnel wind speed is 0.5 m/s or less, for example, is not suitable for the upper and lower wall surfaces of the contraction section 5 as in the wind tunnel of this embodiment. By providing an appropriate number of openings 12 with a cross-sectional area, the wind in the high temperature layer, that is, the acceleration region layer, and the wind in the low temperature layer, that is, the low velocity region layer in the upper or lower layer are discharged to the outside of the body, and the air flow in the contraction section 5 is discharged. The opening 12 is opened by the inner cylinder 11 provided inside.
Since the wind flowing out to the measuring part 7 is stably separated from the wind flowing to the measurement part 7, an air flow having a constant speed and a constant direction can be obtained even when there is a temperature difference between the upper and lower parts of the body at a low wind speed.

なお上記実施例では縮流部5の上下壁にのみ開
口部12を設けたが、胴の周囲全域に亘つて開口
部12を配設しても良い。
In the above embodiment, the openings 12 are provided only in the upper and lower walls of the contraction section 5, but the openings 12 may be provided all around the circumference of the body.

また、測定部と内筒とを一体化し、従来の縮流
部をなす胴壁を、該内筒を覆うようにし、その胴
壁後端を測定部の胴壁とわずかな間隙を有するよ
うにして開口部を形成するようにしても良い。
In addition, the measurement section and the inner cylinder are integrated, and the body wall that forms the conventional flow contraction section is made to cover the inner cylinder, and the rear end of the body wall is made to have a slight gap with the body wall of the measurement section. Alternatively, the opening may be formed using the same method.

【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図は第4図の水平断面図、第6図は
本発明の一実施例の風洞内を流れる風を、従来の
ものと対比して示した図、第7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、12:開口部。
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. 5 is a horizontal sectional view of FIG. 4, FIG. 6 is a diagram showing the wind flowing in the wind tunnel according to an embodiment of the present invention in comparison with the conventional one, and FIG. 7 is a diagram showing the measuring section. It is a graph showing the wind speed at the entrance. 3: Rectifier section, 4: Rectifier device, 5: Contraction section, 7:
Measuring part, 11: inner cylinder, 12: opening.

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 within the contraction section, and an opening is provided in the contraction section. Wind tunnel.
JP17601381A 1981-11-02 1981-11-02 Air duct Granted JPS5877633A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17601381A JPS5877633A (en) 1981-11-02 1981-11-02 Air duct

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17601381A JPS5877633A (en) 1981-11-02 1981-11-02 Air duct

Publications (2)

Publication Number Publication Date
JPS5877633A JPS5877633A (en) 1983-05-11
JPS6256454B2 true JPS6256454B2 (en) 1987-11-26

Family

ID=16006191

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17601381A Granted JPS5877633A (en) 1981-11-02 1981-11-02 Air duct

Country Status (1)

Country Link
JP (1) JPS5877633A (en)

Also Published As

Publication number Publication date
JPS5877633A (en) 1983-05-11

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