The performance of 60deg delta wings The effects of leading edge radius and vortex flaps

Motion induced aerodynamics of a pitching delta wing

Vaughan, J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010637 / BLDSC - British Library D...

Aerodynamic improvement of a delta wing in combination with leading edge flaps

Tadateru Ishide
Mao Itazawa

November 2017

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been report...

IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION

D. Gueraiche
S. А. Popov

January 2018

The article explores the possibility of improving the aerodynamic properties of a supercritical-airf...

The performance of 60deg delta wings The effects of leading edge radius on vortex flaps and the wing

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1990

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...

Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps

Rinoie, K.

January 1996

Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...

Experimental studies of vortex flaps and vortex plates part 1 0.53m 60deg delta wing

Rinoie, K.
Stollery, J
Cranfield Inst. of Technology (United Kingdom). Coll. of Aeronautics

January 1991

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CA-R--9113) / BLDSC - Bri...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

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 ...

NOTATION AR Aspect ratio

B K Hu
Prof J L Stou Ery
Cranfield Bedford
Mk Oal England
B K Hu
Prof J L Stollery
C Wing Chord
C Drage Coefficient

January 1989

"The views expressed herein are those of the authors alone and do not necessarily represent tho...

Effects of Leading-Edge Radius on Aerodynamic Characteristics of 50º Delta Wings

Verhaagen, N.G.

January 2010

The study focuses on the effects of the leading-edge radius on the flow over 50º swept delta wing mo...

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...

Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing

Ghazijahani, Mohammad Sharifi
Yavuz, Mehmet Metin

May 2019

The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...

The effect of a high thrust pusher propeller on the flow over a straight wing

Catalano, F
Cranfield Inst. of Technology (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX181264 / BLDSC - British Library D...

Motion induced aerodynamics of a pitching delta wing

Vaughan, J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010637 / BLDSC - British Library D...

Aerodynamic improvement of a delta wing in combination with leading edge flaps

Tadateru Ishide
Mao Itazawa

November 2017

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been report...

IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION

D. Gueraiche
S. А. Popov

January 2018

The article explores the possibility of improving the aerodynamic properties of a supercritical-airf...

The performance of 60deg delta wings The effects of leading edge radius on vortex flaps and the wing

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1990

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...

Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps

Rinoie, K.

January 1996

Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...

Experimental studies of vortex flaps and vortex plates part 1 0.53m 60deg delta wing

Rinoie, K.
Stollery, J
Cranfield Inst. of Technology (United Kingdom). Coll. of Aeronautics

January 1991

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CA-R--9113) / BLDSC - Bri...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

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 ...

NOTATION AR Aspect ratio

B K Hu
Prof J L Stou Ery
Cranfield Bedford
Mk Oal England
B K Hu
Prof J L Stollery
C Wing Chord
C Drage Coefficient

January 1989

"The views expressed herein are those of the authors alone and do not necessarily represent tho...

Effects of Leading-Edge Radius on Aerodynamic Characteristics of 50º Delta Wings

Verhaagen, N.G.

January 2010

The study focuses on the effects of the leading-edge radius on the flow over 50º swept delta wing mo...

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...

Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing

Ghazijahani, Mohammad Sharifi
Yavuz, Mehmet Metin

May 2019

The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...

The effect of a high thrust pusher propeller on the flow over a straight wing

Catalano, F
Cranfield Inst. of Technology (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX181264 / BLDSC - British Library D...

Motion induced aerodynamics of a pitching delta wing

Vaughan, J.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN010637 / BLDSC - British Library D...

Aerodynamic improvement of a delta wing in combination with leading edge flaps

Tadateru Ishide
Mao Itazawa

November 2017

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been report...

IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION

D. Gueraiche
S. А. Popov

January 2018

The article explores the possibility of improving the aerodynamic properties of a supercritical-airf...

The performance of 60deg delta wings The effects of leading edge radius and vortex flaps

Abstract

Extracted data

The performance of 60deg delta wings The effects of leading edge radius and vortex flaps

Abstract

Extracted data

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