Trailing edge strips to reduce the drag of slender wings

The edges of things

Hodgson, John Terence
University of Sussex (United Kingdom)

January 2002

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN055713 / BLDSC - British Library ...

The stability of the boundary layer on swept wings

Taylor, M.J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199865 / BLDSC - British Library Doc...

Vortex shedding from optical fibres

Webster, S

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97954 / BLDSC - British Library Do...

The control of trailing edge separation on highly swept wings using vortex generators

Broadley, J.I.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN025142 / BLDSC - British Library D...

Induced drag and wake structures behind wings

Lam, F

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:D60893 / BLDSC - British Library Doc...

Some effects of sweep direction and strakes for wings with sharp leading edges

Poll, D.I.A.
Cheng-Hao, Q
Cranfield Inst. of Tech. (CIT), Bedford (United Kingdom). Coll. of Aeronautics

January 1984

7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8421) / BLDSC - British ...

Some effects of transpiration on the boundary layer at the leading edge of a swept wing

Smith, A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...

Leading-edge separation from a slender rolling wing-body combination

Jones, I.P.
Royal Aircraft Establishment, Farnborough (UK)

January 1980

SIGLELD:8717.806(RAE-TR--80039) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Variable camber wings for transport aircraft

Rao, A
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX90881 / BLDSC - British Library Do...

An investigation of low-speed wing buffet

Zan, S.J

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D061511 / BLDSC - British Library Do...

To investigate means of reducing added resistance due to the rudder and yawing in oblique weather

Islam, Z

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX86672 / BLDSC - British Library Do...

Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges

Peckham, D.H
Royal Aircraft Establishment, Bedford (United Kingdom)

January 1958

Recently declassifiedAvailable from British Library Document Supply Centre- DSC:7595.50(RAE-AERO--26...

Reduction of aerodynamic drag

Field, J.E.
Wilby, W.A.
Rees, W.G.
Cambridge Univ. (UK). Cavendish Lab.

January 1981

SIGLELD:0678.231F(AD-A--102-064)(microfiche). / BLDSC - British Library Document Supply CentreGBUnit...

The effect of surface suction near the leading edge of a swept-back wing

Poll, D.
Danks, M.
Davies, A
Manchester Univ. (United Kingdom). Dept. of Aeronautical Engineering

January 1992

Also known as Aeronautical Internal report no. 9205Available from British Library Document Supply Ce...

Separated flow past smooth slender bodies

Williams, A.L

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97391 / BLDSC - British Library Do...

The edges of things

Hodgson, John Terence
University of Sussex (United Kingdom)

January 2002

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN055713 / BLDSC - British Library ...

The stability of the boundary layer on swept wings

Taylor, M.J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199865 / BLDSC - British Library Doc...

Vortex shedding from optical fibres

Webster, S

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97954 / BLDSC - British Library Do...

The control of trailing edge separation on highly swept wings using vortex generators

Broadley, J.I.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN025142 / BLDSC - British Library D...

Induced drag and wake structures behind wings

Lam, F

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:D60893 / BLDSC - British Library Doc...

Some effects of sweep direction and strakes for wings with sharp leading edges

Poll, D.I.A.
Cheng-Hao, Q
Cranfield Inst. of Tech. (CIT), Bedford (United Kingdom). Coll. of Aeronautics

January 1984

7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8421) / BLDSC - British ...

Some effects of transpiration on the boundary layer at the leading edge of a swept wing

Smith, A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...

Leading-edge separation from a slender rolling wing-body combination

Jones, I.P.
Royal Aircraft Establishment, Farnborough (UK)

January 1980

SIGLELD:8717.806(RAE-TR--80039) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Variable camber wings for transport aircraft

Rao, A
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX90881 / BLDSC - British Library Do...

An investigation of low-speed wing buffet

Zan, S.J

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D061511 / BLDSC - British Library Do...

To investigate means of reducing added resistance due to the rudder and yawing in oblique weather

Islam, Z

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX86672 / BLDSC - British Library Do...

Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges

Peckham, D.H
Royal Aircraft Establishment, Bedford (United Kingdom)

January 1958

Recently declassifiedAvailable from British Library Document Supply Centre- DSC:7595.50(RAE-AERO--26...

Reduction of aerodynamic drag

Field, J.E.
Wilby, W.A.
Rees, W.G.
Cambridge Univ. (UK). Cavendish Lab.

January 1981

SIGLELD:0678.231F(AD-A--102-064)(microfiche). / BLDSC - British Library Document Supply CentreGBUnit...

The effect of surface suction near the leading edge of a swept-back wing

Poll, D.
Danks, M.
Davies, A
Manchester Univ. (United Kingdom). Dept. of Aeronautical Engineering

January 1992

Also known as Aeronautical Internal report no. 9205Available from British Library Document Supply Ce...

Separated flow past smooth slender bodies

Williams, A.L

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97391 / BLDSC - British Library Do...

The edges of things

Hodgson, John Terence
University of Sussex (United Kingdom)

January 2002

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN055713 / BLDSC - British Library ...

The stability of the boundary layer on swept wings

Taylor, M.J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D199865 / BLDSC - British Library Doc...

Vortex shedding from optical fibres

Webster, S

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97954 / BLDSC - British Library Do...

Trailing edge strips to reduce the drag of slender wings

Abstract

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Trailing edge strips to reduce the drag of slender wings

Abstract

Extracted data

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