CN102533109B - Oil formula of high speed wind tunnel colorful oil flow experiment - Google Patents

Oil formula of high speed wind tunnel colorful oil flow experiment Download PDF

Info

Publication number
CN102533109B
CN102533109B CN 201110415594 CN201110415594A CN102533109B CN 102533109 B CN102533109 B CN 102533109B CN 201110415594 CN201110415594 CN 201110415594 CN 201110415594 A CN201110415594 A CN 201110415594A CN 102533109 B CN102533109 B CN 102533109B
Authority
CN
China
Prior art keywords
oil
colorful
wind tunnel
high speed
flow experiment
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 - Fee Related
Application number
CN 201110415594
Other languages
Chinese (zh)
Other versions
CN102533109A (en
Inventor
张军强
尚金奎
王世红
王鹏
赵民
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.)
AVIC Shenyang Aerodynamics Research Institute
Original Assignee
AVIC Shenyang Aerodynamics Research Institute
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 AVIC Shenyang Aerodynamics Research Institute filed Critical AVIC Shenyang Aerodynamics Research Institute
Priority to CN 201110415594 priority Critical patent/CN102533109B/en
Publication of CN102533109A publication Critical patent/CN102533109A/en
Application granted granted Critical
Publication of CN102533109B publication Critical patent/CN102533109B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention provides an oil formula of a high speed wind tunnel colorful oil flow experiment. Through a series of wind tunnel experiments, a colorful indicator (fluorescent pigment), a carrier oil (N150 mechanical oil) and a diluent (kerosene) are determined, and mass percentage relations of the three materials are determined; colorful oil flow experiment is finished in a high speed wind tunnel (pressure/transonic velocity) environment so as to obtain a colorful oil flow experiment image with high quality; and the colorful oil flow experiment image is used for analyzing airflow state of the model surface so as to realize high speed wind tunnel multi-color oil flow experiment and express one special flowing phenomenon by using different colors.

Description

The formula of oil of high speed wind tunnel colorful oil flow experiment
Technical field
The present invention relates to wind tunnel color oil stream experimental technique, particularly relate to the formula of oil of high speed wind tunnel colorful oil flow experiment.
Background technology
In wind1 tunnel trial, the oil stream test test method that to be some feature of air-flow winding mold type being flowed by means of physical means show with the form of picture.By observing oily stream picture, and carry out topological analysis, can in depth understand essence and the mechanism of flow phenomenon, determine the position and the mode of separating and characteristics of position, the position that shock wave and vortex occur and pneumatic separation that air-flow adheres on model, for the pragmatize experimental data provides foundation, contribute to find the approach that solves some particular problem, also contribute to set up, improve and develop new Aerodynamics.
Oil flows while testing by the coating special at the coated one deck of model surface (oil plant that normally contains trickle trace particle), when blowing test, the shearing stress that the model surface air stream on accompany surface forms promotes the oil plant film of model surface and does the viscosity motion, forms oily flow pattern.By the observation analysis to oily flow pattern, determine the flow state on model.
The oil flow pattern is actually the oil plant film and does the viscosity motion under air-flow promotes, the mobile trace collection of illustrative plates formed at model surface, and on oily flow pattern, the principal character structure is singular point.So-called singular point is exactly the point that frictional stress is zero.The different modes of assembling or dispersing at the singular point place according to friction line, be divided into dissimilar singular point.Common are saddle point, node and three kinds of singular points of spiral points in the oil flow pattern.
Saddle can be seen two groups of oil stain lines, and one group of oil stain line points to saddle point, and another group oil stain line leaves saddle point, and take a line and assemble gradually as asymptotic line, and the existence of saddle point often shows on object plane to have pneumatic separation, as Fig. 1.
The node place can see that a lot of bar oil stain lines converge to a bit, if all oil stain lines all deviate from node, are called and adhere to node; If all oil stain lines all point to node, be called the separation node, as Fig. 2.
Near oil stain line spiral points is rolled onto a bit twist, if all spiral-linees are all to enter spiral points, for separating spiral points; If all spiral points are all from spiral points, for adhering to spiral points.The existence of spiral points shows on object plane to exist spiral vortex, as Fig. 3.
Summary of the invention
The technical problem to be solved in the present invention, be to provide a kind of wind-tunnel polychrome colorful oil flow experiment of realizing showing, shows the formula of oil of the high speed wind tunnel colorful oil flow experiment of some special flow phenomenon with different color.
The technical scheme adopted is:
The formula of oil of high speed wind tunnel colorful oil flow experiment, be comprised of colored indicator, carrier oil plant and thinner, and its formula is directly related with the wind speed of high-speed wind tunnel, and the formula of oil that concrete the test wind is corresponding is as follows by mass percentage:
(1) when 0.3≤M<0.7
Carrier oil plant 29%
Colored indicator 28%
Thinner 43%
(2) when 0.7≤M<0.8
Carrier oil plant 64%
Colored indicator 19%
Thinner 17%
(3) when 0.8≤M<1.2
Carrier oil plant 54%
Colored indicator 32%
Thinner 14%
Above-mentioned carrier oil plant is the N150 machinery oil.
Above-mentioned colored indicator is the China red fluorescence pigment FT-714 that brightness group produces forever; Green fluorescence pigment FT-711; Blue-fluorescence pigment FT-719.
Above-mentioned thinner is kerosene.
Advantage of the present invention is:
1 can be at the coated oil plant that contains the colored indicator of different colours of model different sites, for flowing of display model surface different sites air-flow while carrying out high speed wind tunnel colorful oil flow experiment.
2 colored indicator can be good at showing oily streak line, need to not spray the priming paint for increasing oily stream picture contrast gradient at model surface;
Under 3 different wind conditions, can select different oil to banish ratio, can obtain best oily streak line image.
The accompanying drawing explanation
Fig. 1 is the saddle point schematic diagram.
Fig. 2 a separates the node schematic diagram.
Fig. 2 b adheres to the node schematic diagram.
Fig. 3 separates the spiral points schematic diagram.
Fig. 4 is the high speed wind tunnel colorful oil flow experiment effect picture that uses blue-fluorescence pigment to carry out.
Embodiment
Embodiment mono-
The formula of oil of high speed wind tunnel colorful oil flow experiment:
(1) according to test M=0.5, get the oil plant consumption of estimating in carrier oil plant 29%, colored indicator 28%, thinner 43% and the test of 0.3≤M<0.7 o'clock, determine the consumption of N150 machinery oil, high-visibility pigment and kerosene.
(2) high-visibility pigment weighing
Using absorbent cotton to dip a small amount of kerosene prepares beaker by oil plant and cleans up, after the kerosene volatilization, beaker is placed on electronic balance (or other weighing utensils), open electronic balance, measure appropriate high-visibility pigment with spoon and pour beaker into, until reach needed weight.
(3) N150 machinery oil and kerosene measures
According to definite N150 machinery oil consumption, select appropriate vol to get instrument, measure appropriate N150 machinery oil and inject the oil plant preparation beaker of (2) mentioning.Measuring of kerosene is consistent with the N150 machinery oil.
(4) oil plant stirs
Use stirring rod that the high-visibility pigment and the oil plant that measure are stirred, until high-visibility pigment and oil plant mix.
(5) oil plant of preparation needs standing for some time, to guarantee the abundant loss of bubble in oil plant.Suggestion configures oil plant before being tested about half hour.
(6) dip proper amount of acetone (dehydrated alcohol) by the model surface wiped clean with absorbent cotton or long stapled cotton before the brushing oil plant, after residual acetone vapors away fully, the oil plant for preparing and obtain sufficient standing is brushed equably at model surface, then can be carried out high speed wind tunnel colorful oil flow experiment.
Embodiment bis-
Embodiment bis-and embodiment mono-are basic identical, without part, are M=0.7, get the carrier oil plant 64% of 0.7≤M<0.8 o'clock, colored indicator 19%, and thinner 17%, other are identical.
Embodiment tri-
Embodiment bis-and embodiment mono-are basic identical, and difference is M=1.18, get the carrier oil plant 54% when 0.8≤M<1.2, colored indicator 32%, and thinner 14%, other is identical.

Claims (4)

1. the formula of oil of high speed wind tunnel colorful oil flow experiment, it is characterized in that being formed by colored indicator, carrier oil plant and thinner, the carrier oil plant adopts the N150 machinery oil, thinner adopts kerosene, its formula is directly related with the wind speed of high-speed wind tunnel, the formula of oil that concrete the test wind is corresponding, as follows by mass percentage:
(1) when 0.3≤M<0.7;
Carrier oil plant 29%;
Colored indicator 28%;
Thinner 43%;
(2) when 0.7≤M<0.8;
Carrier oil plant 64%;
Colored indicator 19%;
Thinner 17%;
(3) when 0.8≤M<1.2;
Carrier oil plant 54%;
Colored indicator 32%;
Thinner 14%.
2. the formula of oil of high speed wind tunnel colorful oil flow experiment according to claim 1, is characterized in that described carrier oil plant is the N150 machinery oil.
3. the formula of oil of high speed wind tunnel colorful oil flow experiment according to claim 1, is characterized in that described colored indicator is red fluorescence pigment FT-714; Green fluorescence pigment FT-711; Blue-fluorescence pigment FT-719.
4. the formula of oil of high speed wind tunnel colorful oil flow experiment according to claim 1, is characterized in that described thinner is kerosene.
CN 201110415594 2011-12-14 2011-12-14 Oil formula of high speed wind tunnel colorful oil flow experiment Expired - Fee Related CN102533109B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110415594 CN102533109B (en) 2011-12-14 2011-12-14 Oil formula of high speed wind tunnel colorful oil flow experiment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110415594 CN102533109B (en) 2011-12-14 2011-12-14 Oil formula of high speed wind tunnel colorful oil flow experiment

Publications (2)

Publication Number Publication Date
CN102533109A CN102533109A (en) 2012-07-04
CN102533109B true CN102533109B (en) 2013-12-25

Family

ID=46341193

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110415594 Expired - Fee Related CN102533109B (en) 2011-12-14 2011-12-14 Oil formula of high speed wind tunnel colorful oil flow experiment

Country Status (1)

Country Link
CN (1) CN102533109B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102889974B (en) * 2012-09-27 2015-10-14 上海交通大学 The proving installation of joint-cutting gas flowfield structure in laser cutting process
CN104087159B (en) * 2014-07-08 2016-05-11 中国空气动力研究与发展中心低速空气动力研究所 A kind of low-speed wind tunnel fluoroleum stream display methods based on emulsion carriers formula
CN106908214B (en) * 2017-03-10 2019-06-21 中国空气动力研究与发展中心高速空气动力研究所 High-speed wind tunnel oil stream tests the configuration method and test finish of finish
CN106840576A (en) * 2017-03-10 2017-06-13 中国空气动力研究与发展中心高速空气动力研究所 High-speed wind tunnel oil stream test method
CN108510474B (en) * 2018-03-09 2021-07-06 上海烟草集团有限责任公司 Method and system for evaluating quality of tobacco leaf image, memory and electronic equipment
CN108489703A (en) * 2018-03-23 2018-09-04 西北工业大学 A kind of colorful oil flow formula suitable for high-speed wind tunnel for clearly demarcating range of Mach numbers
CN108469332A (en) * 2018-03-29 2018-08-31 中国空气动力研究与发展中心高速空气动力研究所 A kind of wind-tunnel oil stream image processing method, apparatus and system
CN108760225A (en) * 2018-04-03 2018-11-06 西北工业大学 A kind of oil stream formula of the high-speed wind tunnel oil stream experiment of clearly calibration range of Mach numbers
CN108896270A (en) * 2018-04-03 2018-11-27 西北工业大学 A kind of oil stream formula of low-speed wind tunnel oil stream experiment that clearly demarcating range of Mach numbers
CN108982052A (en) * 2018-04-03 2018-12-11 西北工业大学 A kind of colorful oil flow formula of low-speed wind tunnel oil stream experiment that clearly demarcating range of Mach numbers
CN110987356A (en) * 2019-12-06 2020-04-10 中国航空工业集团公司沈阳空气动力研究所 Formula and using method of colored oil flow suitable for subsonic velocity temporary flushing wind tunnel
CN111811769B (en) * 2020-06-16 2021-08-06 南京航空航天大学 Three-dimensional internal rotation type air inlet channel real-time oil flow display method with wave-rider precursor
CN112432755B (en) * 2020-10-23 2022-04-12 中国空气动力研究与发展中心高速空气动力研究所 Wide-speed-range color fluorescent oil flow reagent and viscosity adjusting method thereof

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1218076A (en) * 1997-11-24 1999-06-02 中国石油化工总公司 Wax composition for durably dustproofing metal products

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008045451A1 (en) * 2006-10-10 2008-04-17 Applechem Inc Novel natural oil gels and their applications

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1218076A (en) * 1997-11-24 1999-06-02 中国石油化工总公司 Wax composition for durably dustproofing metal products

Also Published As

Publication number Publication date
CN102533109A (en) 2012-07-04

Similar Documents

Publication Publication Date Title
CN102533109B (en) Oil formula of high speed wind tunnel colorful oil flow experiment
CN102564723B (en) Formula of oil for color oil flow test of low-speed wind tunnel
CN106908214B (en) High-speed wind tunnel oil stream tests the configuration method and test finish of finish
CN104849018A (en) Three-component oil for colorful oil flow test of low-speed wind tunnel
CN104849017A (en) Two-component oil for colorful oil flow test of low-speed wind tunnel
CN103728300B (en) Method for measuring methylene blue (MB) value of machine-made sand
CN106092420A (en) The method indirectly measuring electromotor effective push
Barnwell et al. Natural laminar flow and laminar flow control
CN111024361A (en) Device and method for measuring internal resistance of ventilation force measurement test model
CN106840576A (en) High-speed wind tunnel oil stream test method
CN108489703A (en) A kind of colorful oil flow formula suitable for high-speed wind tunnel for clearly demarcating range of Mach numbers
CN103257094B (en) Determination method for dispersibility of carbon nano-tubes in resin
CN105240004A (en) Method for measuring microscopic remaining oil after water flooding of natural rock core
Diebold et al. Aerodynamics of a swept wing with ice accretion at low Reynolds number
CN104390761A (en) Oil formula for fluorescent oil flow friction force field measuring experiments of low-speed wind tunnels
CN108896270A (en) A kind of oil stream formula of low-speed wind tunnel oil stream experiment that clearly demarcating range of Mach numbers
CN108254506A (en) A kind of offline exhaust contaminant transient behavior method measuring device of gasoline car
CN105548000A (en) Method for testing friction-resistant color fastness of pigment for calligraphy and painting
Huyssen et al. Wing-body circulation control by means of a fuselage trailing edge
CN108760225A (en) A kind of oil stream formula of the high-speed wind tunnel oil stream experiment of clearly calibration range of Mach numbers
CN102854118B (en) Magnetic suspension concentration content calibration samples
CN110987356A (en) Formula and using method of colored oil flow suitable for subsonic velocity temporary flushing wind tunnel
CN108982052A (en) A kind of colorful oil flow formula of low-speed wind tunnel oil stream experiment that clearly demarcating range of Mach numbers
CN104087159B (en) A kind of low-speed wind tunnel fluoroleum stream display methods based on emulsion carriers formula
CN207019908U (en) A kind of fuel oil single injector radial distribution experimental rig

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20131225

Termination date: 20171214

CF01 Termination of patent right due to non-payment of annual fee