GB2142290A - Wind tunnels - Google Patents
Wind tunnels Download PDFInfo
- Publication number
- GB2142290A GB2142290A GB08317536A GB8317536A GB2142290A GB 2142290 A GB2142290 A GB 2142290A GB 08317536 A GB08317536 A GB 08317536A GB 8317536 A GB8317536 A GB 8317536A GB 2142290 A GB2142290 A GB 2142290A
- Authority
- GB
- United Kingdom
- Prior art keywords
- walls
- wind tunnel
- ventilated
- working section
- suction
- 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
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
- G01M9/04—Details
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
For the circumstance when a wind tunnel model 7 in a ventilated tunnel generates such suction that air is drawn in via the ventilation, inevitably spoiling readings in a cone converging rapidly behind the model, this invention provides for suction on the ventilations from outside the working section together with a convergent working area. Slots 2 in the walls 1 open into plenum chambers 3 from which air may be drawn by pumps 5. The flexible walls 1 are adjustable by jacks 6. <IMAGE>
Description
SPECIFICATION
Improvements in wind tunnels
The present invention relates to wind tunnels.
It is particularly concerned with wind tunnels of the type having ventilated walls in the working section.
When ventilated wind tunnels are used to test models which generate suction right out to one or more of ventilated walls, air is drawn into the working section through the wall. The effects of this ingression can spread inwards quite rapidly downstream of the model and seriously affect the validity of any readings taken in the tunnel.
By the present invention means are provided in a ventilated wind tunnel for preventing ingression of fluid through the walls.
A ventilated working section wind tunnel according to the present invention has:
a convergent working section,
means for imposing a suction on the ventilated walls from outside the working section.
According to a feature of the invention the distribution of suction is arranged so as to minimise the interference flow camber and corrections to the gradient of free stream
Mach number in use.
Advantageously the invention is realized in a wind tunnel wherein at least two opposing working section walls are flexible. Preferably the region behind the ventilations is compartmentalised so that different air pressure regimes can be established at different parts of ventilated walls. Insofar as this implies a plenum chamber or chambers behind the ventilated walls the outer wall to the plenum chamber or chambers may also be mobile.
A wind tunnel in accordance with the present invention will now be described by way of example with reference to the accompanying drawing, which is a schematic longitudinal section of a wind tunnel working area.
The drawing illustrates a wind tunnel working area having mobile ventilated side walls 1 in sections 1 a. The ventilation comprises slots 2 behind which there are plenum chambers 3 with associated air pumps 4 and gauges 5.
The sections 1 a are arranged for movement to a variety of stations by hydraulic jacks 6. The drawing also shows a model wing 7 in the tunnel working section.
In operation of the wind tunnel when a low pressure is to be generated by the model 7 which will extend to the walls 1, the sections 1 a are adjusted to a convergent configuration as shown and suction is applied to the plenum chambers 3 to give an approximation to a flow with minimum wall interference.
1. A ventilation working section wind tunnel having
a convergent working section, and
means for imposing a suction on the ventilated walls from outside the working section.
2. A wind tunnel as claimed in claim 1 and wherein the means for imposing a suction is adapted so to distribute suction as to minimise interference flow camber and correction to the gradient of free stream Mach number in use.
3. A wind tunnel as claimed in claim 1 or claim 2 and having opposing working section walls which are flexible.
4. A wind tunnel as claimed in any one of claims 1 to 3 and wherein the region behind the ventilations is compartmentalised so that different air pressure regimes can be established at different parts of ventilated walls.
5. A wind tunnel as claimed in any one of the preceding claims and having flexible plenum chamber outer walls.
6. A wind tunnel substantially as hereinbefore described with reference to the accompanying drawing.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (6)
1. A ventilation working section wind tunnel having
a convergent working section, and
means for imposing a suction on the ventilated walls from outside the working section.
2. A wind tunnel as claimed in claim 1 and wherein the means for imposing a suction is adapted so to distribute suction as to minimise interference flow camber and correction to the gradient of free stream Mach number in use.
3. A wind tunnel as claimed in claim 1 or claim 2 and having opposing working section walls which are flexible.
4. A wind tunnel as claimed in any one of claims 1 to 3 and wherein the region behind the ventilations is compartmentalised so that different air pressure regimes can be established at different parts of ventilated walls.
5. A wind tunnel as claimed in any one of the preceding claims and having flexible plenum chamber outer walls.
6. A wind tunnel substantially as hereinbefore described with reference to the accompanying drawing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08317536A GB2142290B (en) | 1983-06-28 | 1983-06-28 | Wind tunnels |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08317536A GB2142290B (en) | 1983-06-28 | 1983-06-28 | Wind tunnels |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8317536D0 GB8317536D0 (en) | 1983-08-03 |
GB2142290A true GB2142290A (en) | 1985-01-16 |
GB2142290B GB2142290B (en) | 1986-08-06 |
Family
ID=10544918
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08317536A Expired GB2142290B (en) | 1983-06-28 | 1983-06-28 | Wind tunnels |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2142290B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0515278A1 (en) * | 1991-05-24 | 1992-11-25 | E.R.é.M.E. | Device for simulating ground movement in aerodynamic wind tunnels |
FR2682435A1 (en) * | 1987-02-25 | 1993-04-16 | Onera (Off Nat Aerospatiale) | Method and device for reducing the noise of a subsonic flow |
US5627312A (en) * | 1995-12-22 | 1997-05-06 | The Boeing Company | Variable resistance ventilated adaptive wind tunnel walls |
CN106404339A (en) * | 2016-11-28 | 2017-02-15 | 中国航空工业集团公司沈阳空气动力研究所 | Clipping wallboard device for transonic-speed test section |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104655392A (en) * | 2015-02-13 | 2015-05-27 | 北京瑞赛长城航空测控技术有限公司 | Synchronous control system and method for all flexible plate nozzle of wind tunnel |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB714169A (en) * | 1951-10-09 | 1954-08-25 | Bristol Aeroplane Co Ltd | A method of and device for producing a flow of compressible fluid |
US3552202A (en) * | 1968-11-13 | 1971-01-05 | Us Air Force | Windtunnel for vtol and stol aircraft models |
US3602920A (en) * | 1969-12-31 | 1971-09-07 | Nasa | Wind tunnel test section |
US3853003A (en) * | 1973-07-13 | 1974-12-10 | Nasa | Wind tunnel flow generation section |
-
1983
- 1983-06-28 GB GB08317536A patent/GB2142290B/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB714169A (en) * | 1951-10-09 | 1954-08-25 | Bristol Aeroplane Co Ltd | A method of and device for producing a flow of compressible fluid |
US3552202A (en) * | 1968-11-13 | 1971-01-05 | Us Air Force | Windtunnel for vtol and stol aircraft models |
US3602920A (en) * | 1969-12-31 | 1971-09-07 | Nasa | Wind tunnel test section |
US3853003A (en) * | 1973-07-13 | 1974-12-10 | Nasa | Wind tunnel flow generation section |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2682435A1 (en) * | 1987-02-25 | 1993-04-16 | Onera (Off Nat Aerospatiale) | Method and device for reducing the noise of a subsonic flow |
EP0515278A1 (en) * | 1991-05-24 | 1992-11-25 | E.R.é.M.E. | Device for simulating ground movement in aerodynamic wind tunnels |
FR2676815A1 (en) * | 1991-05-24 | 1992-11-27 | Serv Souffleries In Et Const | IMPROVEMENT FOR AERODYNAMIC BLOWERS WITH A DEVICE FOR SIMULATING FLOWING SOILS. |
US5627312A (en) * | 1995-12-22 | 1997-05-06 | The Boeing Company | Variable resistance ventilated adaptive wind tunnel walls |
CN106404339A (en) * | 2016-11-28 | 2017-02-15 | 中国航空工业集团公司沈阳空气动力研究所 | Clipping wallboard device for transonic-speed test section |
CN106404339B (en) * | 2016-11-28 | 2018-09-07 | 中国航空工业集团公司沈阳空气动力研究所 | A kind of transonic-test section slicing wallboard device |
Also Published As
Publication number | Publication date |
---|---|
GB2142290B (en) | 1986-08-06 |
GB8317536D0 (en) | 1983-08-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |