CN1603772A - RT and RM instability generation device for fluid interface - Google Patents
RT and RM instability generation device for fluid interface Download PDFInfo
- Publication number
- CN1603772A CN1603772A CN 200410090861 CN200410090861A CN1603772A CN 1603772 A CN1603772 A CN 1603772A CN 200410090861 CN200410090861 CN 200410090861 CN 200410090861 A CN200410090861 A CN 200410090861A CN 1603772 A CN1603772 A CN 1603772A
- Authority
- CN
- China
- Prior art keywords
- section
- fluid interface
- generating means
- experimental section
- instability
- 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.)
- Granted
Links
Images
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
This invention discloses a fluid interface RT and RM instability generating apparatus, which comprises pipes. The said pipes comprises gas section and test section which are sealed and connected with each other, wherein, the gas section is sealed on top and the test section is located with a separate film on bottom. The above structure can conveniently realize the instability experiments of RT and RM in fluid interface.
Description
Technical field
The present invention relates to a kind of fluid interface instability generating means, belong to the fluid mechanics research field.
Background technology
When the interface of being made up of the different fluid of two-layer density is quickened suddenly, this interface can produce scratches and instability, research to this phenomenon not only has wide industrial application values, and on On Basic Research of Fluid Mechanics important academic values is arranged also.This instability is called as Rayleigh-Taylor (RT) instability, and for example, the water surface of ocean is unstability under action of gravity.When this interface was quickened by a shock wave, the instability of this moment was called as Richtmyer-Meshkov (RM) instability, for example, and inertial confinement fusion (ICF).During research ICF, the RM instability process in the time of must knowing shock wave by the interface between high flexible linear-shaped charge and the nuclear fuel.Present popular way is to carry out numerical simulation with supercomputer.Yet, how to verify that these calculation procedures are the problems that must solve.Adopt the mode of high flexible linear-shaped charge blast, not only test costlyly, and be difficult to collect the data that will write down in the blast process.Carry out RT and RM experiment with gas/water termination, can realize density than being instability interface about 1000 times, can be to a certain extent than near the interface conditions among the ICF.Yet, the present device that above-mentioned simulated experiment also do not occur realizing preferably.
Summary of the invention
The objective of the invention is at above-mentioned present situation, provide a kind of compact conformation, easy to use, can make fluid interface RT and RM instability generating means that fluid column moment quickens.
For achieving the above object, technical scheme of the present invention is as follows:
A kind of fluid interface RT and RM instability generating means, it is characterized in that: this device is made up of body, and described body comprises gas section and experimental section, and this gas section and experimental section are tightly connected, wherein gas section upper end sealing, the experimental section lower end is provided with a barrier film.
Further, described experimental section lower end is sealedly connected with discharge section, this discharge section lower end sealing.
Further, the two ends of described experimental section are tightly connected by flange and described gas section and discharge section respectively.
Further, place a thin plate on the described barrier film, the shape of this thin plate is identical with the cross sectional shape of described experimental section, and its size is slightly less than the cross section of this experimental section inwall.
Further, described gas section is divided into two sections, connects by flange seal between the two sections.
Further, the joint flange place between the described gas section two sections is provided with a barrier film, by this barrier film described gas section is divided into hyperbaric chamber and low-pressure chamber.
Further, described device also comprises support, and described body is fixed on this support.
Further, described support upper end is provided with a panel, and panel is provided with and the identical hole of cross sectional shape, described hyperbaric chamber, and upper end, described hyperbaric chamber has external thread and stretch out in the hole passed on the described panel, and pad and setting nut are nested with on it.
Further, described support is provided with hinge, and described experimental section is movably hinged on this support by this hinge.
Further, on described experimental section, be provided with view window.
Further, described low-pressure chamber and experimental section cross sectional shape are square.
Further, on the sidewall of described hyperbaric chamber gas admittance valve and tensimeter are installed.
After adopting said structure, because instability generating means of the present invention comprises support, gas section, experimental section, connected by flange seal between each section, easy for installation, compact conformation can be realized simulated experiment easily; On the other hand,, can directly be communicated with between two sections or be divided into two Room, therefore, can easily realize the RT of fluid interface, the instability simulated experiment of RM dual mode quickly by barrier film because two sections of being connected by flange of gas section form.In addition, because discharge section is closed container, the noise that produces in the time of more can reducing fluid column and fall to discharging at a high speed.And the hinge that the setting nut of hyperbaric chamber upper end is connected with the experimental section side is convenient laborsaving when this device is installed and used.Low-pressure chamber is selected different shapes with experimental section, can realize fluid interface RT and the simulated experiment of RM instability that cross sectional shape is different.
Description of drawings
Fig. 1 is a structural drawing of the present invention;
Fig. 2 is the vertical view of panel of the present invention.
Embodiment:
Further specify the present invention below in conjunction with accompanying drawing.
As shown in Figure 1, the present invention is made up of support 1 and body, and described body comprises gas section 2, experimental section 3, discharge section 4 three parts.
Support 1 is for having the metal frame of certain rigidity, and its upper end is provided with a panel 11, and as shown in Figure 2, panel is provided with hole 12, and the shape in hole 12 is identical with the cross sectional shape of described gas section 2, and this support middle and lower part is provided with hinge 13.
Scratching of producing when the different fluid column of cross sectional shape falls at a high speed is different, and for satisfying the research needs under the different situations, above-mentioned low-pressure chamber 22 and experimental section 3 also can be made as the cross section and be circular or oval-shaped body.This analogue means can carry out the simulated experiment that 50 normal atmospheres are depressed, so the each part mentioned above body is made by the material that can bear greater than 50 standard atmospheric pressures.
In experimentation, open gas admittance valve 25, make gases at high pressure enter high pressure section 21, at this moment the gaseous tension in the low-pressure chamber 22 remains on 1 atmospheric pressure, when tensimeter 26 shows that pressure arrives setting value, valve-off.Under the gases at high pressure effect, barrier film 23 between hyperbaric chamber and the low-pressure chamber is crushed, gases at high pressure impact downwards, producing shock wave acts on the fluid column in the experimental section 3, being crushed fluid column at surge pressure effect lower diaphragm plate 6 by transient state falls at a high speed, on view window 32, place high-speed camera, take when fluid column falls at a high speed under the shock wave effect scratching that the fluid column surface is produced to study.Because of being placed with thin plate 7 on the barrier film 6, make fluid column bottom surface maintenance level in dropping process, more can satisfy the needs of simulated experiment.Fluid column, the barrier film that crushes and the thin plate that falls falls into discharge section 4 together at a high speed, and the simulated experiment of fluid interface RM instability generating process finishes.
If in above-mentioned experimentation, between flange 211,221, barrier film 23 is not set, even hyperbaric chamber 21 communicates with low-pressure chamber 22, open gas admittance valve 25, make gases at high pressure enter gas section 2, when tensimeter 26 shows that pressure arrives setting value, valve-off.The quasistatic gases at high pressure act on the fluid column in the experimental section 3, under ever-increasing gaseous tension effect, barrier film 6 is crushed fluid column suddenly and is fallen at a high speed, on view window 32, place high-speed camera, take scratching of being produced on the fluid column surface when fluid column falls at a high speed, can realize the simulated experiment of fluid interface RT instability generating process to study.
Claims (12)
1, a kind of fluid interface RT and RM instability generating means, it is characterized in that: this device is made up of body, and described body comprises gas section and experimental section, and this gas section and experimental section are tightly connected, wherein gas section upper end sealing, the experimental section lower end is provided with a barrier film.
2, fluid interface RT as claimed in claim 1 and RM instability generating means, it is characterized in that: described experimental section lower end is sealedly connected with discharge section, this discharge section lower end sealing.
3, fluid interface RT as claimed in claim 1 or 2 and RM instability generating means is characterized in that: the two ends of described experimental section are tightly connected by flange and described gas section and discharge section respectively.
4, fluid interface RT as claimed in claim 3 and RM instability generating means is characterized in that: place a thin plate on the described barrier film, the shape of this thin plate is identical with the cross sectional shape of described experimental section, and its size is slightly less than the cross section of this experimental section inwall.
5, fluid interface RT as claimed in claim 4 and RM instability generating means, it is characterized in that: described gas section is divided into two sections, connects by flange seal between the two sections.
6, fluid interface RT as claimed in claim 5 and RM instability generating means is characterized in that: the joint flange place between the described gas section two sections is provided with a barrier film, by this barrier film described gas section is divided into hyperbaric chamber and low-pressure chamber.
7, fluid interface RT as claimed in claim 6 and RM instability generating means, it is characterized in that: described device also comprises support, described body is fixed on this support.
8, fluid interface RT as claimed in claim 7 and RM instability generating means, it is characterized in that: described support upper end is provided with a panel, panel is provided with and the identical hole of cross sectional shape, described hyperbaric chamber, stretch out in the hole that has external thread on the described hyperbaric chamber and pass on the described panel, and pad and setting nut are nested with on it.
9, fluid interface RT as claimed in claim 8 and RM instability generating means, it is characterized in that: described support is provided with hinge, and described experimental section is movably hinged on this support by this hinge.
10, fluid interface RT as claimed in claim 9 and RM instability generating means is characterized in that: be provided with view window on described experimental section.
11, fluid interface RT as claimed in claim 10 and RM instability generating means, it is characterized in that: described low-pressure chamber and experimental section cross sectional shape are square.
12, fluid interface RT as claimed in claim 11 and RM instability generating means is characterized in that: on the sidewall of described hyperbaric chamber gas admittance valve and tensimeter are installed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB200410090861XA CN100362330C (en) | 2004-11-16 | 2004-11-16 | RT and RM instability generation device for fluid interface |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB200410090861XA CN100362330C (en) | 2004-11-16 | 2004-11-16 | RT and RM instability generation device for fluid interface |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1603772A true CN1603772A (en) | 2005-04-06 |
CN100362330C CN100362330C (en) | 2008-01-16 |
Family
ID=34667230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB200410090861XA Expired - Fee Related CN100362330C (en) | 2004-11-16 | 2004-11-16 | RT and RM instability generation device for fluid interface |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN100362330C (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101726402B (en) * | 2009-12-10 | 2011-06-22 | 中国工程物理研究院流体物理研究所 | RM instability precise experiment system for film-free heavy-air column interface |
CN102759439A (en) * | 2012-06-26 | 2012-10-31 | 中国科学技术大学 | Interface generation device for shock tube experimental study |
CN105164757A (en) * | 2013-03-06 | 2015-12-16 | 牛津大学技术转移公司 | Localised energy concentratoin |
US9530524B2 (en) | 2010-05-07 | 2016-12-27 | Oxford University Innovation Limited | Localised energy concentration |
US9620247B2 (en) | 2009-11-27 | 2017-04-11 | Oxford University Innovation Limited | Energy focussing |
US9704603B2 (en) | 2009-11-27 | 2017-07-11 | Oxford University Innovation Limited | High velocity droplet impacts |
US9984774B2 (en) | 2013-03-06 | 2018-05-29 | Oxford University Innovation Limited | Localised energy concentration |
US10155212B2 (en) | 2012-05-21 | 2018-12-18 | Oxford University Innovation Limited | Producing a localized concentration of gas between a surface of a depression and an impacting jet that is formed by using static pressure to collapse a gas pocket |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4430890A (en) * | 1982-05-14 | 1984-02-14 | The United States Of America As Represented By The Secretary Of The Navy | Two layer hydraulic analogy method for testing supersonic gas flows with shock waves |
-
2004
- 2004-11-16 CN CNB200410090861XA patent/CN100362330C/en not_active Expired - Fee Related
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9620247B2 (en) | 2009-11-27 | 2017-04-11 | Oxford University Innovation Limited | Energy focussing |
US9704603B2 (en) | 2009-11-27 | 2017-07-11 | Oxford University Innovation Limited | High velocity droplet impacts |
CN101726402B (en) * | 2009-12-10 | 2011-06-22 | 中国工程物理研究院流体物理研究所 | RM instability precise experiment system for film-free heavy-air column interface |
US9530524B2 (en) | 2010-05-07 | 2016-12-27 | Oxford University Innovation Limited | Localised energy concentration |
US10265674B2 (en) | 2010-05-07 | 2019-04-23 | Oxford University Innovation Limited | Producing a localized compression of gas between a concave surface and an impacting jet that is formed by using a shockwave to collapse a gas pocket |
US10315180B2 (en) | 2010-05-07 | 2019-06-11 | Oxford University Innovation Limited | Localised energy concentration |
US10155212B2 (en) | 2012-05-21 | 2018-12-18 | Oxford University Innovation Limited | Producing a localized concentration of gas between a surface of a depression and an impacting jet that is formed by using static pressure to collapse a gas pocket |
CN102759439A (en) * | 2012-06-26 | 2012-10-31 | 中国科学技术大学 | Interface generation device for shock tube experimental study |
CN102759439B (en) * | 2012-06-26 | 2014-10-15 | 中国科学技术大学 | Interface generation device for shock tube experimental study |
CN105164757A (en) * | 2013-03-06 | 2015-12-16 | 牛津大学技术转移公司 | Localised energy concentratoin |
US9984775B2 (en) | 2013-03-06 | 2018-05-29 | Oxford University Innovation Limited | Localised energy concentration |
US9984774B2 (en) | 2013-03-06 | 2018-05-29 | Oxford University Innovation Limited | Localised energy concentration |
Also Published As
Publication number | Publication date |
---|---|
CN100362330C (en) | 2008-01-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1603772A (en) | RT and RM instability generation device for fluid interface | |
CN103995093B (en) | Power system for coal and gas outburst power effect simulation experiment | |
CN103630540B (en) | Coal petrography gas adsorption-dilatational strain optical metrology instrument | |
CN201285392Y (en) | Mold for coal and firedamp projecting simulator experiment | |
CN102507865A (en) | Simulation test system of coal-gas outburst during rock cross-cut coal uncovering | |
CN104407108A (en) | Integrated coal and gas adsorption and desorption and outstanding test device and test method | |
CN101419146A (en) | Coal and mash gas extrusion mold | |
CN109098693B (en) | Electromagnetic control's high pressure bubble source device under water | |
CN102288506A (en) | Supersonic gas-solid two-phase flow erosive wear test device | |
CN109115958B (en) | Underwater high-pressure gas continuous blasting device and experimental platform | |
CN108825849B (en) | A kind of valve protection mechanism | |
CN203858240U (en) | Power system for coal and gas outburst power effect simulation experiment | |
CN110326942B (en) | Show shelf with multi-angle is vwatched | |
CN218166461U (en) | Molecular sieve oxygen generator convenient for replacing adsorption material | |
CN108169455B (en) | Filling medium true triaxial penetration instability test room and test method | |
CN210375618U (en) | Test device for simulating liquid overflow after catastrophic failure of storage tank | |
CN114458258A (en) | A choke manifold for pressure release is prevented to oil well | |
CN206046586U (en) | A kind of portable deashing device in mine | |
CN220556056U (en) | Gas pressure reducing valve | |
CN110834828B (en) | Anti-shaking liquid storage system with self-cleaning porous medium layer | |
CN204287148U (en) | Unitary coal and gas adsorption desorb and outstanding test unit | |
CN218326214U (en) | Pneumatic film regulating valve | |
CN114062146A (en) | Method and device for simulating low-gravity test of star soil | |
CN208816101U (en) | A kind of high undersea hydrostatic pressures bubble source device of Electromagnetic Control | |
CN2610162Y (en) | Active harmony liquid column damper controlled by screw propeller |
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 | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080116 Termination date: 20101116 |