JPH11237303A - Controller for blowoff type wind tunnel - Google Patents

Abstract

PROBLEM TO BE SOLVED: To make it possible to efficiently set the Reynold's number Re of a measurement part and to prevent a body to be tested and a wind tunnel balance from being applied with an excessive shock due to the change of air current state in the beginning of a wind tunnel test. SOLUTION: According to values representing the Reynold's number set value Re of the measurement part 8, the Mach number set value M of the measurement part, and all temperatures T0a, T0b.K2 of a collection tunnel 6, a total pressure arithmetic circuit 39 derives the target total pressure P01 of the collection tunnel and then the opening degree of a pressure governor valve 5 is controlled. In the starting period W0 of the wind tunnel test, the total temperature T0a set by a total temperature setter 24 is used. Consequently, an abrupt change in air current state exerting adverse influence on the wind tunnel test is prevented. Then variation in the Raynold's number due to variation in the total temperature is reduced by using the value T0b.K2 obtained by multiplying the values of a total temperature conversion coefficient K2(=T0a/T0b1), held by a holding circuit 26 using the total temperature T0b1 detected at a switching point t3 of time, and the total temperature T0b detected by the total temperature detector 23 by a multiplier 36.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a control device for a blow-out type wind tunnel, and more particularly to a device for controlling a Reynolds number of a measuring unit.

[0002]

2. Description of the Related Art A wind tunnel test facility is a test facility widely used for testing various aerodynamic characteristics of a specimen.
Above all, the blow-out type wind tunnel has features such as the ability to easily create high-speed airflow and the ability to increase the total pressure.
It is a test facility often used for aerodynamic characteristics tests of aircraft and rockets. In this blowout type wind tunnel, if the cross-sectional area of the measurement section is increased, there is a problem that the ventilation time required for the test cannot be secured unless the high-pressure storage tank is enlarged.
Therefore, due to conditions such as construction costs and operating costs, the size of the model serving as a sample is reduced, and the cross-sectional area of the measurement unit is reduced.
In this case, the Reynolds number, which is an aerodynamic similarity rule, may be used as a ventilation condition in order to estimate the difference between the actual size and the model size from a wind tunnel test. That is, in the blowout type wind tunnel, aerodynamic characteristics can be measured by blowing high-pressure air stored in the high-pressure storage tank into the wind tunnel. Generally, a model reduced in size to an actual machine is used as a specimen as described above, and a specimen having an actual size is rarely used.
In this case, the Reynolds number, which is an aerodynamic similarity rule, is used as a ventilation condition for wind tunnel operation in order to correct the difference in dimensions.

[0003] The Reynolds number can be expressed as a function of total pressure, total temperature and Mach number once the model dimensions are determined.
In the blow-out type wind tunnel, the total pressure can be adjusted by a pressure regulating valve, and the Mach number can be adjusted by a Mach number adjusting actuator such as a variable nozzle as a first throat, a second throat, a bleed flap, a bleed valve, etc. Temperature cannot be adjusted. Therefore, the resulting total temperature is measured, and after the ventilation, the Reynolds number is calculated.

Conventionally, a wind tunnel operator predicts the total temperature from the temperature of the high-pressure storage tank and the atmospheric temperature, and calculates the total pressure by calculating the total pressure from the predicted total temperature and the desired Reynolds number and Mach number. Driving a wind tunnel as a value. The escape of high-pressure air from the high-pressure storage tank causes a polytropic change in the high-pressure storage tank, so that the temperature of the high-pressure storage tank decreases with ventilation and the total temperature of the collecting cylinder also decreases. Therefore, the Reynolds number differs between the early stage of ventilation and the last stage of ventilation. Generally, the angle of attack of the specimen is changed during ventilation, so that the Reynolds number changes while the angle of attack is changed. Therefore, it is necessary to estimate the aerodynamic characteristics from several ventilations. Under such circumstances, there is a demand for a Reynolds number control device for a blow-out type wind tunnel that can set the Reynolds number efficiently.

A prior art for solving this problem is disclosed in Japanese Patent Publication No. Hei 5-37264 (JP-A-62-39742). In this prior art, an approximate value of the total pressure in the measuring section is calculated by a calculator from the measured value of the total temperature in the collecting cylinder in the blow-out type wind tunnel, the set value of the Reynolds number, and the set value of the Mach number. In order to realize the value, the opening of the pressure regulating valve is controlled, thereby keeping the Reynolds number in the measuring section approximately at the set value. A new problem of this prior art is that, at the beginning of the wind tunnel test, i.e., immediately after the wind tunnel is started, the total temperature in the collecting cylinder fluctuates greatly, and as a result, the total pressure in the measuring section fluctuates greatly. Therefore, in the early stage of the wind tunnel test, the airflow state in the measuring section changes suddenly, which results in an excessive impact on the aircraft model and the balance, which are the specimens. Therefore, the rigidity of the specimen and the wind tunnel balance is increased so that the specimen can withstand an excessive impact. Increasing the rigidity of the specimen makes it difficult to manufacture and expensive. When the rigidity of the balance is increased, the detection sensitivity is reduced, and it becomes impossible to accurately collect necessary data.

[0006]

SUMMARY OF THE INVENTION It is an object of the present invention to make it possible to efficiently set the Reynolds number in a measuring section and to prevent an excessive impact due to a sudden change in air flow on a specimen in the measuring section. An object of the present invention is to provide a control device for a blow-out type wind tunnel.

[0007]

SUMMARY OF THE INVENTION According to the present invention, there is provided an air storage tank for storing a compressed gas, a collecting cylinder to which the gas from the storage tank is guided, a gas to be guided from the collecting cylinder, and a specimen to be installed. In a control device of a blow-out type wind tunnel having a measuring section and a pressure regulating valve provided on the upstream side of the collecting cylinder and having a variable opening degree and a fully closed function, the total temperature for detecting the total temperature T0b of the collecting cylinder A detector, a total temperature setter for setting the total temperature T0a of the collecting cylinder, and total temperatures set as the detected total temperatures T0b and T0b1 in response to respective outputs of the total temperature detector and the total temperature setter. A coefficient calculation circuit for calculating the total temperature conversion coefficients K1 and K2, which is a ratio with respect to T0a; a hold circuit for holding the output from the coefficient calculation circuit in response to a command signal; The total temperature T0a set by the heater is derived and After, it provides an instruction signal to the hold circuit, the whole temperature conversion coefficient K which is held in the hold circuit
1, K2, and the total temperature T detected by the total temperature detector.
Switching operation means for deriving a value multiplied by 0b and T0b1, a Reynolds number setting device for setting the Reynolds number of the measurement section, a Mach number setting device for setting the Mach number of the measurement section, switching operation means and Reynolds number A total pressure calculating circuit for calculating the total pressure P01 of the collecting cylinder, a total pressure detector for detecting the total pressure P02 of the collecting cylinder, and a total pressure calculating circuit in response to each output of the setting device and the Mach number setting device And control means for controlling the opening of the pressure regulating valve so that the total pressure P02 detected by the collecting cylinder is equal to the set total pressure P01 in response to each output of the total pressure detector. This is a control device for a blow-out type wind tunnel.

According to the present invention, the Reynolds number Re in the measuring section is determined by the total pressure P02 of the collecting cylinder, the Mach number M of the measuring section, and the total temperature T0b of the collecting cylinder. The Reynolds number is set by the Reynolds setting device, the Mach number is set by the Mach number setting device, the total temperature T0b of the collecting cylinder is detected, and the total pressure P02 of the collecting cylinder is changed to the total pressure P01 of the collecting cylinder by the switching operation means. Thus, the opening of the pressure regulating valve is controlled.

In the early stage of the wind tunnel test, the airflow is unstable and the total temperature of the collecting cylinder fluctuates greatly. At the time of starting the wind tunnel, the total pressure P01 for controlling the opening of the pressure regulating valve is set using the constant total temperature T0a of the collecting cylinder set by the total temperature setting device. This prevents the set value of the total pressure of the collecting cylinder from fluctuating.

After that, after the airflow becomes stable and the time rate of change of the total temperature of the collecting cylinder becomes small, the total temperature T0b of the collecting cylinder detected by the total temperature detector is used.
Negative feedback control of the total pressure P02 of the collecting cylinder is performed, and the total pressure P0
2 controls the opening degree of the pressure regulating valve so that the total pressure P01 becomes the set total pressure P01. At the time of switching by the switching operation means, the set total temperature T0a and the multiplied value, that is, the total temperature become close to each other, whereby the total pressure of the collecting cylinder does not greatly fluctuate. Can be ventilated while the Reynolds number is kept substantially constant.

In this way, the fluctuation of the Reynolds number Re due to the fluctuation of the total temperature T0b of the collecting cylinder is moderated. Further, a value substantially approximate to the Reynolds number set by the Reynolds number setting device can be realized, and the Reynolds number can be kept constant.

A pressure regulating valve having a fully closed function may be configured with a shut-off valve interposed on the storage tank side of the pressure regulating valve itself whose opening degree is variable, that is, on the upstream side. , The concept of a pressure regulating valve having a fully closed function.

Further, according to the present invention, the switching operation means includes a multiplier for multiplying the total temperature T0b detected by the total temperature detector by the total temperature conversion coefficient K2 held in the hold circuit, and a total temperature setter. Set total temperature T0a
Switching means for switching and outputting the output of the multiplier;
Timing control means for deriving the set total temperature T0a by the switching means at the initial stage of the wind tunnel test, thereafter deriving a command signal and supplying the command signal to the hold circuit, and deriving the output of the multiplier by the switching means. It is characterized by the following.

According to the present invention, as shown in FIGS. 1 and 2 to be described later, it includes a multiplier, a switching means, and a timing control means. The total temperature T0a is directly supplied to the total pressure calculation circuit via the switching means, and the total pressure P0 as a target of the collecting cylinder is obtained.
1 is calculated.

According to the present invention, the switching operation means multiplies the total temperature T0b detected by the total temperature detector by the input signals T0a / T0b and K2, and derives the multiplied outputs T0a and T0a1. Multiplier for giving to the total temperature arithmetic circuit, output means T0a / T0b of the coefficient arithmetic circuit, and switching means for giving an output signal K2 of the hold circuit as the input signal of the multiplier. Timing control means for deriving the output T0a / T0b of the arithmetic circuit by the switching means, thereafter deriving a command signal and applying it to the hold circuit, and deriving the output K2 of the hold circuit by the switching means. .

According to the present invention, as shown in FIG. 3 described later, the switching operation means includes a multiplier, a switching means, and a timing control means, and at the beginning of the wind tunnel test, a coefficient operation circuit is provided in the multiplier. And the total temperature T0b of the collecting cylinder detected by the total temperature detector. As a result, the total temperature T0a set by the total temperature setting device is calculated and given to the total pressure calculation circuit, and the total pressure P as the target of the collecting cylinder is calculated.
01 is calculated.

[0017]

FIG. 1 is a system diagram showing the overall configuration of an embodiment of the present invention. In the blow-out type wind tunnel 1, a compressed gas, for example, compressed air is sent from the compressor 3 into the high-pressure storage tank 2. The compressed air in the air storage tank 2 is
Through the pressure regulating valve 5 to the collecting cylinder 6. The collecting cylinder 6 has a variable nozzle 7 having an adjustable opening degree as a first throat.
Through the measuring unit 8. Downstream of the measuring unit,
The second throat 9 and the diffusion cylinder 10 are connected.

In the pressure regulating valve 5, the valve body 11 can adjust the cross-sectional area of the passage between the valve body 11 and the valve seat 12, that is, the opening degree thereof.
The valve closing function can be achieved by the valve body 11 sitting on the valve seat 12. The valve body 11 can be driven to be displaced by the driving means 13. Thereby, the opening can be controlled as described above.

In another embodiment of the present invention, in order to achieve the valve closing function, an openable / closable shutoff valve is interposed in the middle of the pipe 4, and an opening degree between the valve body 11 and the valve seat 12 is provided. May be adjusted, and the shutoff valve may achieve the valve closing function. Such a configuration is also included in the spirit of the present invention.

The measuring section 8 includes a porous wall 14 having air permeability.
Defines the measuring unit 8. A test piece 59 is provided in the measuring section 8. The wind tunnel balance is provided in the measuring unit 8 and is used to measure the force around the coordinate axis of the specimen 59 and the moment of the six-component force. The measurement unit 8 is provided with a bleed flap 15 that can be opened and closed by a hinge 60. Further, a part of the flap 16 of the porous wall 14 can be opened and closed by a hinge 17. A plenum chamber 19 is formed by the housing 18 surrounding the measurement section 8 and the bleed flap 15. A bleed valve 20 is connected to the plenum chamber 19, and a pipe 21 communicates with the atmosphere. In the plenum chamber 19, air flows out from the inside of the measuring section 8 through a large number of holes formed in the porous wall 14, the air is temporarily stopped in the plenum chamber 19, and the air is stopped downstream of the measuring section 8. Then, it is merged with the main flow in the measuring section 8 via the bleed flap 15. The degree of opening of the bleed flap 15 and the flap 16 of the porous wall 14 can be controlled by an actuator. The purpose of opening the flap 16 is not to make the air flow out, but to make the circuit section of the measuring section larger.

The total pressure P02 of the collecting cylinder 6 is applied to the collecting cylinder 6.
Is provided. The collecting cylinder 6 is also provided with a total temperature detector 23 for detecting the total temperature T0b. Further, a total temperature setting device 24 for setting the total temperature T0a of the collecting cylinder 6 is provided. The coefficient operation circuit 25 responds to each output of the total temperature detector 23 and the total temperature setter 24,
A total temperature conversion coefficient K1, which is a ratio between the detected total temperature T0b and the set total temperature T0a, is calculated.

K1 = T0a / T0b (1) The output from the coefficient operation circuit 25 is given to a hold circuit 26 realized by a memory, for example. The hold circuit 26 holds, holds, and stores the output of the coefficient calculation circuit 25 in response to the command signal via the line 27.

An operation signal generating circuit 29 for deriving an operation signal for a wind tunnel test is provided. This operation signal is provided to a command signal generation circuit 31 in the switching calculation means 30.
The command signal generation circuit 31 constitutes a timing control unit. The command signal generating circuit 31 responds to the operation signal and generates a command signal on the line 27 after an elapse of an initial period W0 (see FIG. 2 described later) of the wind tunnel test.

This command signal is supplied to the hold circuit 26 as described above and also to the changeover switch 32. The hold circuit 26 controls the total temperature detector 23 at time t3 (see FIG. 2 described later) when the command signal is given.
The total temperature conversion coefficient K2 is obtained using the total temperature T0b1 detected by (1).

K2 = T0a / T0b1 (2) The changeover switch 32 has a common contact 33 and two individual contacts 34 and 35. The individual contact 34 is supplied with a signal indicating the total temperature T0a from the total temperature setter 24. The output from the multiplier 36 is given to another individual contact 35. The multiplier 36 is provided with the total temperature T0b detected by the total temperature detector 23 and the total temperature conversion coefficient K2 held by the hold circuit 26.
・ Calculate K2. The changeover switch 32 is connected to the line 27
In the initial period W0 during which no command signal is supplied, the common contact 33 is made conductive to the individual contact 34, and the common signal 33 is switched to the individual contact 35 to be conductive when the command signal is supplied.

The Reynolds number setting device 37 sets the Reynolds number Re of the measuring section 8. The Mach number setting device 38 sets the Mach number M of the measuring unit 8. The total pressure calculation circuit 39
In response to the signal from the common contact 33 of the changeover switch 32, the output of the Reynolds number setting device 37, and the output of the Mach number setting device 38, the calculation of the Reynolds number-to-total pressure conversion is performed according to Equation 3.

[0027]

(Equation 1)

Here, P01 is the total pressure to be the target of the collecting cylinder 6, and T0 is the common contact 3 of the changeover switch 32.
3 is the total temperature T0a or T0b · K2 represented by the signal provided via line 40, κ is the specific heat ratio of the compressed air as a gas, and μ0 is the ratio of the compressed air as a gas at the total temperature T0. Viscosity coefficient, R is gas constant.
This Equation 3 is disclosed in “Aerospace Technology Laboratory Report TR-647” issued by the Aerospace Technology Laboratory.

A signal representing the target total pressure P01 derived from the total pressure calculation circuit 39 via a line 41 is supplied to a subtractor 42. The output of the total pressure detector 22 is also provided to the subtractor 42 via a line 43. PID
The (proportional, integral, differential) control circuit 44 responds to the output of the subtractor 42 and is supplied from a line 45 to one individual contact 47 of a changeover switch 46. The changeover switch 46 is provided with another individual contact 48. The changeover switch 46 connects these individual contacts 47 and 48 to a common contact 49.
To conduct. The output of the common contact 49 is provided to the driving means 13, which drives the valve body 11 of the pressure regulating valve 5 to displace, controls the opening of the pressure regulating valve 5, and
Is in the fully closed state.

The individual contacts 48 of the changeover switch 46 include:
A fully closed signal for bringing the pressure regulating valve 5 into a fully closed state is provided from a fully closed signal generation circuit 50. This changeover switch 46
When the operation signal is not supplied from the operation signal generation circuit 29, the common contact 49 is electrically connected to the individual contact 48, whereby the pressure regulating valve 5 is fully closed. When the operation signal is supplied to the changeover switch 46, the common contact 49 conducts to the individual contact 47 during the wind tunnel test, the signal on the line 45 is supplied to the driving means 13, and the opening of the pressure regulating valve 5 is controlled. Is done.

The operation of the embodiment shown in FIG. 1 will be described with reference to FIG. At the start of the wind tunnel test, the operation signal generation circuit 29 generates an operation signal that continues from time t1 to time t4, which is the period of the wind tunnel test, as shown in FIG. Before time t1, the common contact 49 of the changeover switch 46 is electrically connected to the individual contact 48, whereby the pressure regulating valve 5 is fully closed. Operation signal generation circuit 2
9 generates an operation signal that lasts from time t1 to t4 as described above, as shown in FIG. Thereby, the common contact 49 of the changeover switch 46 is connected to the individual contact 4
Switch to 7.

In the switching operation means 30, the command signal generation circuit 31 outputs a signal at line t, as shown in FIG. 2 (2), at time t1 after the lapse of the initial period W0 from time t1.
3 to generate a command signal that lasts until time t4. In the initial period W0, the command signal 27 is not generated,
At this time, the common contact 33 of the changeover switch 32 is electrically connected to the individual contact 34. Therefore, the signal indicating the set total temperature T0a from the total temperature setting device 24 is supplied to the total pressure calculation circuit 39 via the changeover switch 32. The total pressure calculation circuit 39 performs a calculation according to the above-described Expression 3. This causes the control circuit 44 to make the total pressure P02 detected by the total pressure detector 22 reach and match the target total pressure P01 to be derived by the total pressure calculation circuit 39 to the line 41. Is output to a line 45. A control signal derived from the control circuit 44 to a line 45 is as follows:
It is provided to the driving means 13 via the changeover switch 46, and thus the opening of the pressure regulating valve 5 is controlled. The temperature T0b detected by the total temperature detector 23 of the collecting cylinder 6 is shown in FIG.
It changes as shown in (3). The total pressure P02 detected by the total pressure detector 22 changes as shown in FIG. At time t2 shown in FIG. 2 (3), the total temperature T0b of the collecting cylinder 6 becomes the maximum, and thereafter, the total temperature T0b
0b gradually decreases with time. The total pressure P02 detected by the collecting cylinder 6 is maintained at a substantially constant target total pressure P01 after time t3 as shown in FIG. 2 (4). The initial period W0 is, for example, 3 to
6 seconds, and time t1 to time t4 is about 1 minute. In this initial period W0, the total temperature T0b of the collecting cylinder 6 detected
Suddenly changes and is unstable, and the detected total temperature P02 also fluctuates greatly with time.

Thereafter, at time t3, the command signal generating circuit 31 generates a command signal, whereby the common contact 33 of the changeover switch 32 is switched to the individual contact 35. This command signal is also provided to the hold circuit 26. The hold circuit 26 stores, in the hold circuit 26, the total temperature conversion coefficient K2 calculated by Expression 2 using the temperature T0b1 detected by the total temperature detector 23 at time t3.

In this way, the changeover switch 3
The second individual contact 35 has a total temperature T0a1
Is derived and supplied to the total pressure calculation circuit 39 via the changeover switch 32.

T0a1 = T0b · K2 (4) The total temperature conversion coefficient K2 held by the hold circuit 26
Is the value at time t3 as described above, and is kept constant until time t4 when the wind tunnel test ends. Thus, at time t3 at the time of switching, the set total temperature T0a
And the fluctuation of the total pressure P02 of the collecting cylinder 6 due to the difference from the total temperature T0a1 after the initial period W0, and hence the fluctuation of the number of Reynolds nozzles Re, and keeping the air at a constant Reynolds number Re at time t3. Can be.

FIG. 3 is a block diagram showing the overall configuration of another embodiment of the present invention. This embodiment is similar to the embodiment of FIGS. 1 and 2 described above, and corresponding parts are denoted by the same reference numerals. It should be noted that in this embodiment, in the switching operation means 52, the multiplier 36 converts the total temperature T0b detected by the total temperature detector 23 and the signal input from the changeover switch 54 via the line 53. The product is multiplied, and the multiplied output is supplied to a total pressure calculating circuit 39 from a line 40. The common contact 55 of the changeover switch 54 is switched to the individual contacts 56 and 57 to conduct.
The output of the coefficient calculation circuit 25 is given to the individual contact 56. The output of the hold circuit 26 is given to another individual contact 57. The output of the common contact 55 of the changeover switch 54 is provided as an input signal of the multiplier 36 via the line 53 as described above. The command signal from command signal generating circuit 31 is applied to changeover switch 54 and to hold circuit 26.

The switch 54 keeps the common contact 55 electrically connected to the individual contact 56 during the period when no command signal is given, and this state is maintained during the initial period W0. In a period from time t3 in FIG. 2 to time t4 when the wind tunnel test ends, the changeover switch 5
4 switches the common contact 55 to the individual contact 57 in response to the command signal.
Is kept conductive. Therefore, as in the above-described embodiment, in the initial period W0 of the wind tunnel test, the total temperature conversion coefficient K1 represented by the above equation 1 is derived from the coefficient calculation circuit 25 and multiplied from the line 53 via the changeover switch 54. To the vessel 36. Therefore, the product T0b · K1 of the total temperature T0b detected by the total temperature detector 23 and the total temperature conversion coefficient K1 represented by the equation 1, and the set value T0a of the total temperature, is derived from the multiplier 36 to the line 40. Is done. After the time t3, the hold circuit 26 holds the total temperature conversion coefficient K2 expressed by the above-described equation 2, and the multiplier 3
6 given. Thus, the line 40 is output from the multiplier 36.
Then, a signal representing the total temperature T0a1 represented by the above equation 4 is derived. Other configurations and operations are the same as those of the above-described embodiment.

[0038]

According to the first aspect of the present invention, in the initial stage of the wind tunnel test, the airflow at the time of starting the wind tunnel is disturbed, and during the period when the total temperature of the collecting cylinder fluctuates greatly, the temperature is set by the total temperature setting device. The total temperature is given to the total pressure calculation circuit together with the Reynolds number set by the Reynolds number setter and the Mach number set by the Mach number setter, and the target total pressure P01 of the collecting cylinder is calculated and obtained. This prevents the total pressure P01 of the collecting cylinder from fluctuating, and enables the control means to stably control the opening of the pressure regulating valve.

Thereafter, after time t3 when the airflow in the collecting cylinder is stabilized, negative feedback control of the pressure regulating valve is performed by using the total temperature T0b of the collecting cylinder detected by the total temperature detector, and the switching operation means is switched. During operation, both the set total temperature T0a and the multiplied value from the switching operation means, that is, the total temperature, are close to each other, thereby eliminating large fluctuations in the opening of the pressure regulating valve. The hold circuit is
For example, the switching time t3 is realized by a memory or the like.
, The total temperature conversion coefficient K2 calculated by the coefficient calculation circuit using the detected total temperature T0b1 is held, held, and stored at the switching time, so that the Reynolds number at the switching time t3 is maintained constant thereafter. Can be ventilated.

In this way, the Reynolds number can be set efficiently, and a sudden change in the airflow state can be prevented, so that an excessive impact is not given to the specimen and the balance. Thus, it is not necessary to increase the rigidity of the specimen, and the production of the specimen can be facilitated and the cost can be reduced. Further, since it is not necessary to increase the rigidity of the wind tunnel balance, the sensitivity can be improved and highly accurate data can be collected.

According to the second aspect of the present invention, as shown in FIGS. 1 and 2, during the initial period W0 of the wind tunnel test, the total temperature T0a from the total temperature setter is directly changed to the total temperature via the switching means. The operation is given to the pressure operation circuit, and the operation can be simplified.

According to the third aspect of the present invention, as shown in FIG. 3 described above, the multiplier is provided with a total temperature conversion coefficient K1 which is an output of the coefficient operation circuit, via a switching means, and a holding circuit. The total temperature conversion coefficient K2 held at the switching time t3, which is the output, is switched and given. In this way, the calculation result of the coefficient calculation circuit is commonly used in the total pressure calculation circuit in the initial period W0 of the wind tunnel test and thereafter, and the multiplier is commonly used. Therefore, it is easy to find a malfunction at the time of failure or the like.

[Brief description of the drawings]

FIG. 1 is a system diagram showing an overall configuration of an embodiment of the present invention.

FIG. 2 describes the operation of the embodiment shown in FIG.

FIG. 3 is a block diagram showing an overall configuration of another embodiment of the present invention.

[Explanation of symbols]

 REFERENCE SIGNS LIST 1 blow-out type wind tunnel 2 air storage tank 3 compressor 5 pressure regulating valve 6 collecting cylinder 7 variable nozzle 8 measuring unit 9 second throat 11 valve body 12 valve seat 15 bleed flap 19 plenum chamber 20 bleed valve 22 total pressure detector 23 total temperature Detector 24 Total temperature setting device 25 Coefficient operation circuit 26 Hold circuit 29 Operation signal generation circuit 30, 52 Switching operation means 31 Command signal generation circuit 32, 46, 54 Changeover switch 36 Multiplier 37 Reynolds number setting device 38 Mach number setting device 39 Total pressure operation circuit 42 Subtractor 44 Control circuit 50 Fully closed signal generation circuit 59 Specimen

Claims (3)

[Claims] 1. A gas storage tank for storing compressed gas, a collecting cylinder to which gas from the storage tank is guided, a measuring unit to which a gas is guided from the collecting cylinder and a specimen is installed, A control device for a blow-out type wind tunnel provided on the upstream side and having a pressure regulating valve having a variable opening degree and a fully closed function, comprising: a total temperature detector for detecting a total temperature T0b of the collecting cylinder; A total temperature setter for setting the temperature T0a, and a total temperature T0 set as the detected total temperatures T0b and T0b1 in response to respective outputs of the total temperature detector and the total temperature setter.
a coefficient calculation circuit for calculating the total temperature conversion coefficients K1 and K2, which is a ratio to a, a hold circuit for holding the output from the coefficient calculation circuit in response to a command signal, and setting the total temperature at the beginning of the wind tunnel test The total temperature T0a set by the temperature detector is derived, and then a command signal is given to the hold circuit to convert the total temperature conversion coefficients K1 and K2 held by the hold circuit and the total temperatures T0b and T0b1 detected by the total temperature detector. Switching operation means for deriving a value obtained by multiplying the above, a Reynolds number setting device for setting the Reynolds number of the measurement section, a Mach number setting device for setting the Mach number of the measurement section, switching operation means and the Reynolds number setting device, A total pressure calculating circuit that calculates a total pressure P01 of the collecting cylinder in response to each output of the Mach number setting device, a total pressure detector that detects a total pressure P02 of the collecting cylinder, and a total pressure calculating circuit. Control means for controlling the opening of the pressure regulating valve in response to each output from the total pressure detector so that the detected total pressure P02 of the collecting cylinder becomes the set total pressure P01. The control device of the wind tunnel. 2. The switching operation means includes a multiplier for multiplying a total temperature T0b detected by a total temperature detector by a total temperature conversion coefficient K2 held by a hold circuit, and a total temperature setter. Switching means for switching and deriving the total temperature T0a and the output of the multiplier; and deriving the set total temperature T0a by the switching means at the initial stage of the wind tunnel test, and thereafter deriving a command signal to the hold circuit. 2. A control device for a blow-out type wind tunnel according to claim 1, further comprising timing control means for providing the output of said multiplier by switching means. 3. The switching operation means multiplies the total temperature T0b detected by the total temperature detector by the input signals T0a / T0b, K2, derives the multiplied outputs T0a, T0a1, and derives the total temperature. A multiplier to be applied to the arithmetic circuit; switching means for switching between the output T0a / T0b of the coefficient arithmetic circuit and the output K2 of the hold circuit to provide the input signal of the multiplier; and the initial stage of the wind tunnel test, Output T0a / T
2. A blow-off device according to claim 1, further comprising timing control means for deriving 0b by a switching means, thereafter deriving a command signal and supplying the command signal to a hold circuit, and deriving an output K2 of the hold circuit by the switching means. Wind tunnel control device.