The 30 x 30 inch wind tunnel

Aerofoil testing in a self-streamlining flexible walled wind tunnel

Lewis, M.C

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D81901 / BLDSC - British Library Doc...

Wind tunnel investigation of a pair of ellipsoids in close proximity

Utama, I.
Molland, A.
Southampton Univ. (United Kingdom). Dept. of Ship Science

January 1997

Available from British Library Document Supply Centre-DSC:8258.9254(98) / BLDSC - British Library Do...

Flow calibrations in the Warton 5.5m Low Speed Wind Tunnel

Norris, R.D.
Green, L.G
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:7383.518(ARG--215) / BLDSC - British...

5.5m low speed wind tunnel

Stott, M.R
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:7383.518(BAAG-ARG--205) / BLDSC - Br...

2.7m x 2.1m low speed wind tunnel Water tunnel report

Fisher, J
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:2286.891(BAE-AXM--132) / BLDSC - Bri...

Wind tunnels and test rigs of the Department of Aeronautics, Imperial College

Bradshaw, P
Imperial Coll. of Science and Technology, London (United Kingdom). Dept. of Aeronautics

January 1986

Supersedes IC-AERO--79-05SIGLEAvailable from British Library Document Supply Centre- DSC:4360.17V(IC...

Wind tunnel measurements on a low rise building and comparison with full scale

Dalley, S

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX175986 / BLDSC - British Library D...

The 13ft x 9ft low speed wind tunnel facility at DRA (Aerospace Division) Bedford (UK)

Cripps, M
Defence Research Agency, Bedford (United Kingdom). Aerospace Div

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(DRA-TM-AERO--2228) / BLDSC -...

Wind tunnel tests on a variable camber wing

MacKinnon, A.
Stollery, J
College of Aeronautics, Cranfield (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9304) / BLDSC - Brit...

Near wake wind tunnel studies

Green, D.R.R
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
Loughborough Univ. of Technology (United Kingdom). Dept. of Mechanical Engineering

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.49(ETSU-WN--5040/1) / BLDSC - B...

Full scale wind tunnel tests on hang glider pilots

Kilkenny, E.A
Cranfield Inst. of Tech. (CIT), Bedford (United Kingdom). Coll. of Aeronautics

January 1984

7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8416) / BLDSC - British ...

Wind tunnel investigation of road vehicle wakes

Davis, J.P.

January 1982

SIGLEAvailable from British Library Document Supply Centre-DSC:DX193058 / BLDSC - British Library Do...

A wind-tunnel study of flow over hills

Green, D

January 1983

SIGLEAvailable from British Library Document Supply Centre- DSC:D52444/84 / BLDSC - British Library ...

Aerofoil testing in a self-streaming flexible walled wind tunnel

Lewis, M.C

January 1987

Available from British Library Document Supply Centre- DSC:D82542 / BLDSC - British Library Document...

Main features of Warton 2.7 x 2.1m low speed wind tunnel

British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1985

Issue 1SIGLEAvailable from British Library Document Supply Centre- DSC:2286.891(BAE-AXM--124) / BLDS...

Aerofoil testing in a self-streamlining flexible walled wind tunnel

Lewis, M.C

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D81901 / BLDSC - British Library Doc...

Wind tunnel investigation of a pair of ellipsoids in close proximity

Utama, I.
Molland, A.
Southampton Univ. (United Kingdom). Dept. of Ship Science

January 1997

Available from British Library Document Supply Centre-DSC:8258.9254(98) / BLDSC - British Library Do...

Flow calibrations in the Warton 5.5m Low Speed Wind Tunnel

Norris, R.D.
Green, L.G
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:7383.518(ARG--215) / BLDSC - British...

5.5m low speed wind tunnel

Stott, M.R
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:7383.518(BAAG-ARG--205) / BLDSC - Br...

2.7m x 2.1m low speed wind tunnel Water tunnel report

Fisher, J
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:2286.891(BAE-AXM--132) / BLDSC - Bri...

Wind tunnels and test rigs of the Department of Aeronautics, Imperial College

Bradshaw, P
Imperial Coll. of Science and Technology, London (United Kingdom). Dept. of Aeronautics

January 1986

Supersedes IC-AERO--79-05SIGLEAvailable from British Library Document Supply Centre- DSC:4360.17V(IC...

Wind tunnel measurements on a low rise building and comparison with full scale

Dalley, S

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX175986 / BLDSC - British Library D...

The 13ft x 9ft low speed wind tunnel facility at DRA (Aerospace Division) Bedford (UK)

Cripps, M
Defence Research Agency, Bedford (United Kingdom). Aerospace Div

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(DRA-TM-AERO--2228) / BLDSC -...

Wind tunnel tests on a variable camber wing

MacKinnon, A.
Stollery, J
College of Aeronautics, Cranfield (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9304) / BLDSC - Brit...

Near wake wind tunnel studies

Green, D.R.R
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
Loughborough Univ. of Technology (United Kingdom). Dept. of Mechanical Engineering

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.49(ETSU-WN--5040/1) / BLDSC - B...

Full scale wind tunnel tests on hang glider pilots

Kilkenny, E.A
Cranfield Inst. of Tech. (CIT), Bedford (United Kingdom). Coll. of Aeronautics

January 1984

7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8416) / BLDSC - British ...

Wind tunnel investigation of road vehicle wakes

Davis, J.P.

January 1982

SIGLEAvailable from British Library Document Supply Centre-DSC:DX193058 / BLDSC - British Library Do...

A wind-tunnel study of flow over hills

Green, D

January 1983

SIGLEAvailable from British Library Document Supply Centre- DSC:D52444/84 / BLDSC - British Library ...

Aerofoil testing in a self-streaming flexible walled wind tunnel

Lewis, M.C

January 1987

Available from British Library Document Supply Centre- DSC:D82542 / BLDSC - British Library Document...

Main features of Warton 2.7 x 2.1m low speed wind tunnel

British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1985

Issue 1SIGLEAvailable from British Library Document Supply Centre- DSC:2286.891(BAE-AXM--124) / BLDS...

Aerofoil testing in a self-streamlining flexible walled wind tunnel

Lewis, M.C

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D81901 / BLDSC - British Library Doc...

Wind tunnel investigation of a pair of ellipsoids in close proximity

Utama, I.
Molland, A.
Southampton Univ. (United Kingdom). Dept. of Ship Science

January 1997

Available from British Library Document Supply Centre-DSC:8258.9254(98) / BLDSC - British Library Do...

Flow calibrations in the Warton 5.5m Low Speed Wind Tunnel

Norris, R.D.
Green, L.G
British Aerospace Aircraft Group, Preston (United Kingdom). Military Aircraft Div

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:7383.518(ARG--215) / BLDSC - British...

The 30 x 30 inch wind tunnel

Abstract

Extracted data

The 30 x 30 inch wind tunnel

Abstract

Extracted data

Related items

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