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

Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy

Hendrich, T.J.M. (author)

April 2011

Traditionally, the aircraft design process is divided into three phases: conceptual, preliminary and...

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...

High-fidelity Aerostructural Optimization of Nonplanar Wings for Commercial Transport Aircraft

Khosravi, Shahriar

November 2016

Although the aerospace sector is currently responsible for a relatively small portion of global anth...

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...

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
Cranfield Inst. of Tech. (United Kingdom)

January 1986

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

Flow structure and drag influence of a wing/fuselage junction

Kapfer, D

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182385 / BLDSC - British Library D...

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...

Application Of Optimisation Techniques In Aviation Industries

June 2015

In the modern aircraft many components were produced because of the effort of engineering fraternity...

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...

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...

The integration of structural optimization in the general design process for aircraft

Schweiger, J.
Goedel, H.
Lotze, H.
Sensburg, O.
Messerschmitt-Boelkow-Blohm G.m.b.H., Muenchen (Germany). Unternehmensbereich Hubschrauber und Flugzeuge

January 1990

SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...

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...

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...

Glider fuselage-wing junction optimization using CFD and RBF mesh morphing

BIANCOLINI, MARCO EVANGELOS
COSTA, EMILIANO
CELLA, UBALDO
GROTH, CORRADO
Veble, G
Andrejasic, M.

January 2016

Purpose - The present paper aims to address the description of a numerical optimization procedure, b...

Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy

Hendrich, T.J.M. (author)

April 2011

Traditionally, the aircraft design process is divided into three phases: conceptual, preliminary and...

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...

High-fidelity Aerostructural Optimization of Nonplanar Wings for Commercial Transport Aircraft

Khosravi, Shahriar

November 2016

Although the aerospace sector is currently responsible for a relatively small portion of global anth...

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...

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
Cranfield Inst. of Tech. (United Kingdom)

January 1986

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

Flow structure and drag influence of a wing/fuselage junction

Kapfer, D

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182385 / BLDSC - British Library D...

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...

Application Of Optimisation Techniques In Aviation Industries

June 2015

In the modern aircraft many components were produced because of the effort of engineering fraternity...

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...

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...

The integration of structural optimization in the general design process for aircraft

Schweiger, J.
Goedel, H.
Lotze, H.
Sensburg, O.
Messerschmitt-Boelkow-Blohm G.m.b.H., Muenchen (Germany). Unternehmensbereich Hubschrauber und Flugzeuge

January 1990

SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...

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...

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...

Glider fuselage-wing junction optimization using CFD and RBF mesh morphing

BIANCOLINI, MARCO EVANGELOS
COSTA, EMILIANO
CELLA, UBALDO
GROTH, CORRADO
Veble, G
Andrejasic, M.

January 2016

Purpose - The present paper aims to address the description of a numerical optimization procedure, b...

Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy

Hendrich, T.J.M. (author)

April 2011

Traditionally, the aircraft design process is divided into three phases: conceptual, preliminary and...

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...

High-fidelity Aerostructural Optimization of Nonplanar Wings for Commercial Transport Aircraft

Khosravi, Shahriar

November 2016

Although the aerospace sector is currently responsible for a relatively small portion of global anth...

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

Abstract

Extracted data

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

Abstract

Extracted data

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