Plane frame stability analysis based on the inelastic zone method

On the development of computer code for aircraft flight dynamics analysis

Mohamed Alazomui, Outman

December 2014

The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stabilit...

An investigation into the compressive strength and stability characteristics of welded aircraft fuselage panels

Gibson, A.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN036250 / BLDSC - British Library D...

Aeroelastic stability analysis of a bird-damaged fan assembly

Kim, K.
Vahdati, M.
Imregun, M.
Rolls-Royce plc (United Kingdom)

January 2001

Available from British Library Document Supply Centre-DSC:8019.322(92805) / BLDSC - British Library ...

In-plane stability of portal frames to BS 5950-1:2000

King, C.
Steel Construction Inst., Ascot (United Kingdom)

January 2001

Specialist design guidesAvailable from British Library Document Supply Centre-DSC:8127.922(P292) / B...

Geometrically non-linear analysis of plane frames composed of prismatic and tapered sections

Bawa, G.S

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX87261 / BLDSC - British Library Do...

Lateral stability analysis of frames for civilianaircraft structures

Grossmann, Oscar

January 2017

The fuselage of a civilian airplane is a quite complex structure build from slendermembers and panel...

Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression

Murphy, A.

January 2003

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN064106 / BLDSC - British Library ...

Practical advanced analysis for design of laterally unrestrained steel planar frames under in -plane loads

Wongkaew, Kamaiton

January 2000

Currently, advanced analysis procedures that are suitable for practical design of steel planar frame...

Analysis and design of semi-continuous sway and non-sway frames

Fisher, C.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN049196 / BLDSC - British Library D...

Finite element stability analysis of thin-walled steel structures

Nemir, M.T.M

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D66910/86 / BLDSC - British Library ...

Stability of steel frames by the transfer matrix method

Kameshki, E.S

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX172400 / BLDSC - British Library D...

A finite element study of the postbuckling behaviour of a typical aircraft fuselage panel

Lynch, C.J.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN042976 / BLDSC - British Library D...

Global linear stability analysis of thin aerofoil wakes

Peake, N.
Woodley, B.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92350) / BLDSC - British Lib...

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...

Stability analysis of continuum/ skeletal fibre matrix systems

Ishakian, V

January 1980

Available from British Library Document Supply Centre- DSC:D33216/80 / BLDSC - British Library Docum...

On the development of computer code for aircraft flight dynamics analysis

Mohamed Alazomui, Outman

December 2014

The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stabilit...

An investigation into the compressive strength and stability characteristics of welded aircraft fuselage panels

Gibson, A.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN036250 / BLDSC - British Library D...

Aeroelastic stability analysis of a bird-damaged fan assembly

Kim, K.
Vahdati, M.
Imregun, M.
Rolls-Royce plc (United Kingdom)

January 2001

Available from British Library Document Supply Centre-DSC:8019.322(92805) / BLDSC - British Library ...

In-plane stability of portal frames to BS 5950-1:2000

King, C.
Steel Construction Inst., Ascot (United Kingdom)

January 2001

Specialist design guidesAvailable from British Library Document Supply Centre-DSC:8127.922(P292) / B...

Geometrically non-linear analysis of plane frames composed of prismatic and tapered sections

Bawa, G.S

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX87261 / BLDSC - British Library Do...

Lateral stability analysis of frames for civilianaircraft structures

Grossmann, Oscar

January 2017

The fuselage of a civilian airplane is a quite complex structure build from slendermembers and panel...

Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression

Murphy, A.

January 2003

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN064106 / BLDSC - British Library ...

Practical advanced analysis for design of laterally unrestrained steel planar frames under in -plane loads

Wongkaew, Kamaiton

January 2000

Currently, advanced analysis procedures that are suitable for practical design of steel planar frame...

Analysis and design of semi-continuous sway and non-sway frames

Fisher, C.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN049196 / BLDSC - British Library D...

Finite element stability analysis of thin-walled steel structures

Nemir, M.T.M

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D66910/86 / BLDSC - British Library ...

Stability of steel frames by the transfer matrix method

Kameshki, E.S

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX172400 / BLDSC - British Library D...

A finite element study of the postbuckling behaviour of a typical aircraft fuselage panel

Lynch, C.J.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN042976 / BLDSC - British Library D...

Global linear stability analysis of thin aerofoil wakes

Peake, N.
Woodley, B.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92350) / BLDSC - British Lib...

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...

Stability analysis of continuum/ skeletal fibre matrix systems

Ishakian, V

January 1980

Available from British Library Document Supply Centre- DSC:D33216/80 / BLDSC - British Library Docum...

On the development of computer code for aircraft flight dynamics analysis

Mohamed Alazomui, Outman

December 2014

The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stabilit...

An investigation into the compressive strength and stability characteristics of welded aircraft fuselage panels

Gibson, A.

January 2000

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN036250 / BLDSC - British Library D...

Aeroelastic stability analysis of a bird-damaged fan assembly

Kim, K.
Vahdati, M.
Imregun, M.
Rolls-Royce plc (United Kingdom)

January 2001

Available from British Library Document Supply Centre-DSC:8019.322(92805) / BLDSC - British Library ...

Plane frame stability analysis based on the inelastic zone method

Abstract

Extracted data

Plane frame stability analysis based on the inelastic zone method

Abstract

Extracted data

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