The aerodynamic design optimisation of a forward swept wing fighter aircraft

Design synthesis for Canard-delta combat aircraft

Serghides, V.C
Cranfield Inst. of Tech. (United Kingdom)

January 1987

2 volsAvailable from British Library Document Supply Centre- DSC:DX82026 / BLDSC - British Library D...

Multi-disciplinary design of wings for transport aircraft operating at high subsonic speed

Djafri, D.Y.

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN007341 / BLDSC - British Library D...

Vehicle aerodynamics

Royal Aeronautical Society, London (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:f94/0267 / BLDSC - British Library D...

ASTOVL combat aircraft design synthesis and optimization

Kehayas, N
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX98001 / BLDSC - British Library Do...

Design synthesis for swept-wing combat aircraft incorporating stealth technology

Siegers, F
Cranfield College of Aeronautics (United Kingdom). Dept. of Aerospace Technology

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9402) / BLDSC - Brit...

Aeroelastic optimisation of composite wings

Lillico, M.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN013251 / BLDSC - British Library D...

Aircraft trajectory optimisation

Elsayed, M.A.N

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D66055/86 / BLDSC - British Library ...

Quiet aircraft study Aerodynamic considerations of proposed swept shielded aircraft configurations

British Aerospace Aircraft Group, Weybridge (United Kingdom)

January 1972

SIGLEAvailable from British Library Document Supply Centre- DSC:2265.63F(BR--72788) / BLDSC - Britis...

Conceptual design synthesis and optimization for new generations of combat aircraft

Siegers, F
Cranfield Coll. of Aeronautics (United Kingdom). Dept. of Aerospace Science

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(COA--9606) / BLDSC - British...

Aerodynamic design via optimal control theory

Yiu, K.F.C

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:D174483 / BLDSC - British Library Do...

The aerodynamic design and optimization of a wing-fuselage junction fillet as part of a multi-disciplinary optimization process during the early aircraft design stages

Hadjiilias, A.H.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN019308 / BLDSC - British Library D...

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

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

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:DX72266/87 / BLDSC - British Library...

The aerodynamics of slender aircraft forebodies at high angle of attack

Petterson, K.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN049959 / BLDSC - British Library D...

The aerodynamics of high speed aerial weapons

Prince, S.A.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN037231 / BLDSC - British Library D...

Forward Swept Wing Design Study

Ortmann, Judith
Hepperle, Martin

June 2007

One goal of K2020 is the design of a forward swept wing. In the present work a forward swept wing in...

Design synthesis for Canard-delta combat aircraft

Serghides, V.C
Cranfield Inst. of Tech. (United Kingdom)

January 1987

2 volsAvailable from British Library Document Supply Centre- DSC:DX82026 / BLDSC - British Library D...

Multi-disciplinary design of wings for transport aircraft operating at high subsonic speed

Djafri, D.Y.

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN007341 / BLDSC - British Library D...

Vehicle aerodynamics

Royal Aeronautical Society, London (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:f94/0267 / BLDSC - British Library D...

ASTOVL combat aircraft design synthesis and optimization

Kehayas, N
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX98001 / BLDSC - British Library Do...

Design synthesis for swept-wing combat aircraft incorporating stealth technology

Siegers, F
Cranfield College of Aeronautics (United Kingdom). Dept. of Aerospace Technology

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9402) / BLDSC - Brit...

Aeroelastic optimisation of composite wings

Lillico, M.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN013251 / BLDSC - British Library D...

Aircraft trajectory optimisation

Elsayed, M.A.N

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D66055/86 / BLDSC - British Library ...

Quiet aircraft study Aerodynamic considerations of proposed swept shielded aircraft configurations

British Aerospace Aircraft Group, Weybridge (United Kingdom)

January 1972

SIGLEAvailable from British Library Document Supply Centre- DSC:2265.63F(BR--72788) / BLDSC - Britis...

Conceptual design synthesis and optimization for new generations of combat aircraft

Siegers, F
Cranfield Coll. of Aeronautics (United Kingdom). Dept. of Aerospace Science

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(COA--9606) / BLDSC - British...

Aerodynamic design via optimal control theory

Yiu, K.F.C

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:D174483 / BLDSC - British Library Do...

The aerodynamic design and optimization of a wing-fuselage junction fillet as part of a multi-disciplinary optimization process during the early aircraft design stages

Hadjiilias, A.H.

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN019308 / BLDSC - British Library D...

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

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

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:DX72266/87 / BLDSC - British Library...

The aerodynamics of slender aircraft forebodies at high angle of attack

Petterson, K.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN049959 / BLDSC - British Library D...

The aerodynamics of high speed aerial weapons

Prince, S.A.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN037231 / BLDSC - British Library D...

Forward Swept Wing Design Study

Ortmann, Judith
Hepperle, Martin

June 2007

One goal of K2020 is the design of a forward swept wing. In the present work a forward swept wing in...

Design synthesis for Canard-delta combat aircraft

Serghides, V.C
Cranfield Inst. of Tech. (United Kingdom)

January 1987

2 volsAvailable from British Library Document Supply Centre- DSC:DX82026 / BLDSC - British Library D...

Multi-disciplinary design of wings for transport aircraft operating at high subsonic speed

Djafri, D.Y.

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN007341 / BLDSC - British Library D...

Vehicle aerodynamics

Royal Aeronautical Society, London (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:f94/0267 / BLDSC - British Library D...

The aerodynamic design optimisation of a forward swept wing fighter aircraft

Abstract

Extracted data

The aerodynamic design optimisation of a forward swept wing fighter aircraft

Abstract

Extracted data

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