Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

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...

Enhancing lift on a three element high lift aerofoil system by installing air jet vortex generators

Lewington, Neil

January 2001

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN060193 / BLDSC - British Library ...

Mechanisms in wing-in-ground effect aerodynamics

Jones, M.A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN043779 / BLDSC - British Library Docume...

Aeroelastic optimisation of composite wings

Lillico, M.

January 1997

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

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

Souahi, A.

June 1986

The research reported in this thesis is concerned with the structural weight optimization of aircra...

Optimisation of tolerances and manufacturing procedures for aircraft surface features

Sanchez, M.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN043133 / BLDSC - British Library D...

The aerodynamic design optimisation of a forward swept wing fighter aircraft

Cook, M.V.
Heydari, F
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1987

7.50Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--8718) / BLDSC - Brit...

A multi-disciplinary optimisation model for passenger aircraft wing structures with manufacturing and cost considerations

Wang, L.

January 2000

Available from British Library Document Supply Centre-DSC:DXN044749 / BLDSC - British Library Docume...

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...

Aircraft trajectory optimisation

Elsayed, M.A.N

January 1985

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

Strength and Aeroelastic Structural Optimization of Aircraft Lifting Surfaces using Two-Level Approach

Svetlana I. Kuzmina
Vasily V. Chedrik
Fanil Z. Ishmuratov

January 2005

The paper gives brief description of the multidisciplinary design system for aeroelastic and strengt...

Approximate methods for predicting the lifting characteristics of wing-body combinations

Hamwi, S
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX90890 / BLDSC - British Library Do...

On the prospects for increasing dynamic lift

Mabey, D.G
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.2(RAE-TM-AERO--2068) / BLDSC - ...

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...

Multidisciplinary design optimization of aircraft wing structures with aeroelastic and aeroservoelastic constraints.

Jung, Sang-young.

January 1999

Design procedures for aircraft wing structures with control surfaces are presented using multidiscip...

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...

Enhancing lift on a three element high lift aerofoil system by installing air jet vortex generators

Lewington, Neil

January 2001

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN060193 / BLDSC - British Library ...

Mechanisms in wing-in-ground effect aerodynamics

Jones, M.A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN043779 / BLDSC - British Library Docume...

Aeroelastic optimisation of composite wings

Lillico, M.

January 1997

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

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

Souahi, A.

June 1986

The research reported in this thesis is concerned with the structural weight optimization of aircra...

Optimisation of tolerances and manufacturing procedures for aircraft surface features

Sanchez, M.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN043133 / BLDSC - British Library D...

The aerodynamic design optimisation of a forward swept wing fighter aircraft

Cook, M.V.
Heydari, F
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1987

7.50Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--8718) / BLDSC - Brit...

A multi-disciplinary optimisation model for passenger aircraft wing structures with manufacturing and cost considerations

Wang, L.

January 2000

Available from British Library Document Supply Centre-DSC:DXN044749 / BLDSC - British Library Docume...

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...

Aircraft trajectory optimisation

Elsayed, M.A.N

January 1985

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

Strength and Aeroelastic Structural Optimization of Aircraft Lifting Surfaces using Two-Level Approach

Svetlana I. Kuzmina
Vasily V. Chedrik
Fanil Z. Ishmuratov

January 2005

The paper gives brief description of the multidisciplinary design system for aeroelastic and strengt...

Approximate methods for predicting the lifting characteristics of wing-body combinations

Hamwi, S
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX90890 / BLDSC - British Library Do...

On the prospects for increasing dynamic lift

Mabey, D.G
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.2(RAE-TM-AERO--2068) / BLDSC - ...

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...

Multidisciplinary design optimization of aircraft wing structures with aeroelastic and aeroservoelastic constraints.

Jung, Sang-young.

January 1999

Design procedures for aircraft wing structures with control surfaces are presented using multidiscip...

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...

Enhancing lift on a three element high lift aerofoil system by installing air jet vortex generators

Lewington, Neil

January 2001

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN060193 / BLDSC - British Library ...

Mechanisms in wing-in-ground effect aerodynamics

Jones, M.A.

January 2000

Available from British Library Document Supply Centre-DSC:DXN043779 / BLDSC - British Library Docume...

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

Abstract

Extracted data

Structural optimization of aircraft lifting surfaces to satisfy flutter requirements

Abstract

Extracted data

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