GB2142290A - Wind tunnels - Google Patents

Wind tunnels Download PDF

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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
Application number
GB08317536A
Other versions
GB2142290B (en
GB8317536D0 (en
Inventor
Peter Herbert Cook
Michael Charles Peter Firmin
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB08317536A priority Critical patent/GB2142290B/en
Publication of GB8317536D0 publication Critical patent/GB8317536D0/en
Publication of GB2142290A publication Critical patent/GB2142290A/en
Application granted granted Critical
Publication of GB2142290B publication Critical patent/GB2142290B/en
Expired legal-status Critical Current

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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
    • G01M9/02Wind tunnels
    • G01M9/04Details

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  • 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)

**WARNING** start of CLMS field may overlap end of DESC **. 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. CLAIMS
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.
GB08317536A 1983-06-28 1983-06-28 Wind tunnels Expired GB2142290B (en)

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

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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)

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GB (1) GB2142290B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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PCNP Patent ceased through non-payment of renewal fee