Gerard Ernest Andre Jourdain

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Featured researches published by Gerard Ernest Andre Jourdain.

Archive | 1980

Injection device for the combustion chamber of turbine engines

Gerard Ernest Andre Jourdain; Marcel Robert Soligny

Archive | 1990

HEAT PROTECTIVE LINING FOR AN AFTERBURNER OR TRANSITION DUCT OF A TURBOJET ENGINE

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1988

Assembly of two bodies having distinctly different coefficients of expansion

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1980

RETAINING STRUCTURE FOR THE COMPRESSOR HOUSING OF A TURBO ENGINE

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marcel Robert Soligny

Archive | 1988

Assembly method for two parts having different thermal expansion coefficients

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1981

Supersonic nozzle for a turbojet engine

Jean-Marie Ernest Clovis Hardy; Gerard Ernest Andre Jourdain; Marcel Robert Soligny

Archive | 1983

Pressure drop regulating device

Jean Georges Bouiller; Marc François Bernard Buisson; Gerard Ernest Andre Jourdain; Denis Jean Maurice Sandelis; Yves Robert Alfred Urruty

Archive | 1983

DEVICE FOR REGULATING THE PRESSURE DROP ACROSS AT LEAST ONE FLUX OF A MULTIFLUX TURBINE

Jean Georges Bouiller; Marc François Bernard Buisson; Gerard Ernest Andre Jourdain; Denis Jean Maurice Sandelis; Yves Robert Alfred Urruty

Archive | 1990

Heat insulation structure for an afterburner liner or turbine transition piece

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1985

Compressor blow-off arrangement

Jean Georges Bouiller; Gerard Ernest Andre Jourdain

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Archive Network Publication Hotspot Collaboration

Network

Latest external collaboration on country level. Dive into details by clicking on the dots.

Hotspot

Dive into the research topics where Gerard Ernest Andre Jourdain is active.

Publication

Featured researches published by Gerard Ernest Andre Jourdain.

Injection device for the combustion chamber of turbine engines

HEAT PROTECTIVE LINING FOR AN AFTERBURNER OR TRANSITION DUCT OF A TURBOJET ENGINE

Assembly of two bodies having distinctly different coefficients of expansion

RETAINING STRUCTURE FOR THE COMPRESSOR HOUSING OF A TURBO ENGINE

Assembly method for two parts having different thermal expansion coefficients

Supersonic nozzle for a turbojet engine

Pressure drop regulating device

DEVICE FOR REGULATING THE PRESSURE DROP ACROSS AT LEAST ONE FLUX OF A MULTIFLUX TURBINE

Heat insulation structure for an afterburner liner or turbine transition piece

Compressor blow-off arrangement

Collaboration

Dive into the Gerard Ernest Andre Jourdain's collaboration.