Parietal vortex shedding as a cause of instability for long solid propellant motors : numerical simulations and comparisons with firing tests

Numerical computations and visualization tests of the flow inside a cold gas simulation with characterization of a parietal vortex shedding

Avalon, G.
Ugurtas, B.
Grisch, F.
Bresson, A.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

Communication to : 36th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Huntsville (USA)...

Large-Eddy simulation of vortex shedding and pressure oscillations in solid rocket motors

Bernardini M.
Cimini M.
Stella F.
Cavallini E.
Di Mascio A.
Neri A.
Martelli E.

January 2020

A three-dimensional high-fidelity numerical simulation of a small-scale solid rocket motor is carrie...

Vortex Shedding Inside a Baffled Air Duct

Davis, Philip
Kenny, R. Jeremy

December 2010

Common in the operation of both segmented and un-segmented large solid rocket motors is the occurren...

Stability analysis and numerical simulation of simplified solid rocket motors

Boyer, G.
Casalis, G.
Estivalèzes, J.-L.

August 2013

International audienceThis paper investigates the Parietal Vortex Shedding (PVS) instability that si...

Numerical simulation of vortex shedding phenomenon in 2D test case solid rocket motors

Lupoglazoff, N.
Vuillot, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1992

Tire de : 30th AIAA Aerospace sciences meeting, Reno (NV, USA), january 6-9, 1992SIGLEAvailable at I...

Vortex flow analysis of a large segmented solid rocket motor

Prahalad N. Tengli
C. S. Ramesh
K. Viswanathan
R. Saravanan

October 2016

It is not uncommon to find pressure oscillations in large size segmented solid rocket motors. During...

Simulations and linear stability analysis of corner vortex shedding in solid rocket motors

Lacassagne, Laura

April 2017

Les oscillations de pression sont un enjeu majeur dans le design des moteurs à propergol solide car ...

Comparison between firing tests and numerical simulation of vortex shedding in a 2-D test solid motor

Lupoglazoff, Nicolas
Vuillot, Francois
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1993

Communication to : AIAA 24th Fluid Dynamics Conference, Orlando, FL (USA), July 6-9, 1993Available a...

Linear Analysis of Vortex-Shedding Induced Longitudinal Oscillations in Segmented Solid Rocket Motors

CIUCCI A
DAURIA F
D'AGOSTINO L

January 2003

A linear model for the analysis of longitudinal fluid dynamic oscillations in solid rocket motors is...

Numerical simulations of vortex shedding phenomenon in a SRM using two approaches

Schmeisser-Gailliegue, K.
Fabignon, Y.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1996

Communication to : 32nd AIAA/ASME/SAE/ASEE joint propulsion conference, Lake Buena Vista, FL (USA), ...

Convergence of Two Analytical Flow Field Models Predicting a Destabilizing Agent in Rocket Combustion

J. Majdalani
G. A. Fl
T. S. Roh

August 2014

In the combustion stability assessment of solid propellant rocket motors, several new destabilizing ...

Instabilities inside solid rocket motors : influence of the star-shaped geometry and numerical study of the laminar-turbulent transition

Bouyges, Maxime

November 2017

Les moteurs à propergol solide de certains lanceurs spatiaux peuvent présenter des oscillations de p...

Simulations of solid propellant rocket motors instability including propellant combustion response

Lupoglazoff, N.
Vuillot, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : 6th International congress on sound and vibration, Lyngby (Denmark), July 05-08, ...

Instabilités dans les moteurs à propergol solide : influence de la géométrie étoilée et étude numérique de la transition laminaire-turbulent

Bouyges, Maxime

November 2017

Solid rocket motors may exhibit thrust oscillations induced by pressure oscillations inside the engi...

Particle effects on solid-propellant motors flow stability

Feraille, Thierry
Casalis, Gregoire
Dupays, Joel
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2002

Communication to : 38th AIAA/ASME/SAE/ASEE Joint propulsion conference and exhibit, Indianapolis (US...

Numerical computations and visualization tests of the flow inside a cold gas simulation with characterization of a parietal vortex shedding

Avalon, G.
Ugurtas, B.
Grisch, F.
Bresson, A.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

Communication to : 36th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Huntsville (USA)...

Large-Eddy simulation of vortex shedding and pressure oscillations in solid rocket motors

Bernardini M.
Cimini M.
Stella F.
Cavallini E.
Di Mascio A.
Neri A.
Martelli E.

January 2020

A three-dimensional high-fidelity numerical simulation of a small-scale solid rocket motor is carrie...

Vortex Shedding Inside a Baffled Air Duct

Davis, Philip
Kenny, R. Jeremy

December 2010

Common in the operation of both segmented and un-segmented large solid rocket motors is the occurren...

Stability analysis and numerical simulation of simplified solid rocket motors

Boyer, G.
Casalis, G.
Estivalèzes, J.-L.

August 2013

International audienceThis paper investigates the Parietal Vortex Shedding (PVS) instability that si...

Numerical simulation of vortex shedding phenomenon in 2D test case solid rocket motors

Lupoglazoff, N.
Vuillot, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1992

Tire de : 30th AIAA Aerospace sciences meeting, Reno (NV, USA), january 6-9, 1992SIGLEAvailable at I...

Vortex flow analysis of a large segmented solid rocket motor

Prahalad N. Tengli
C. S. Ramesh
K. Viswanathan
R. Saravanan

October 2016

It is not uncommon to find pressure oscillations in large size segmented solid rocket motors. During...

Simulations and linear stability analysis of corner vortex shedding in solid rocket motors

Lacassagne, Laura

April 2017

Les oscillations de pression sont un enjeu majeur dans le design des moteurs à propergol solide car ...

Comparison between firing tests and numerical simulation of vortex shedding in a 2-D test solid motor

Lupoglazoff, Nicolas
Vuillot, Francois
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1993

Communication to : AIAA 24th Fluid Dynamics Conference, Orlando, FL (USA), July 6-9, 1993Available a...

Linear Analysis of Vortex-Shedding Induced Longitudinal Oscillations in Segmented Solid Rocket Motors

CIUCCI A
DAURIA F
D'AGOSTINO L

January 2003

A linear model for the analysis of longitudinal fluid dynamic oscillations in solid rocket motors is...

Numerical simulations of vortex shedding phenomenon in a SRM using two approaches

Schmeisser-Gailliegue, K.
Fabignon, Y.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1996

Communication to : 32nd AIAA/ASME/SAE/ASEE joint propulsion conference, Lake Buena Vista, FL (USA), ...

Convergence of Two Analytical Flow Field Models Predicting a Destabilizing Agent in Rocket Combustion

J. Majdalani
G. A. Fl
T. S. Roh

August 2014

In the combustion stability assessment of solid propellant rocket motors, several new destabilizing ...

Instabilities inside solid rocket motors : influence of the star-shaped geometry and numerical study of the laminar-turbulent transition

Bouyges, Maxime

November 2017

Les moteurs à propergol solide de certains lanceurs spatiaux peuvent présenter des oscillations de p...

Simulations of solid propellant rocket motors instability including propellant combustion response

Lupoglazoff, N.
Vuillot, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : 6th International congress on sound and vibration, Lyngby (Denmark), July 05-08, ...

Instabilités dans les moteurs à propergol solide : influence de la géométrie étoilée et étude numérique de la transition laminaire-turbulent

Bouyges, Maxime

November 2017

Solid rocket motors may exhibit thrust oscillations induced by pressure oscillations inside the engi...

Particle effects on solid-propellant motors flow stability

Feraille, Thierry
Casalis, Gregoire
Dupays, Joel
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2002

Communication to : 38th AIAA/ASME/SAE/ASEE Joint propulsion conference and exhibit, Indianapolis (US...

Numerical computations and visualization tests of the flow inside a cold gas simulation with characterization of a parietal vortex shedding

Avalon, G.
Ugurtas, B.
Grisch, F.
Bresson, A.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

Communication to : 36th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Huntsville (USA)...

Large-Eddy simulation of vortex shedding and pressure oscillations in solid rocket motors

Bernardini M.
Cimini M.
Stella F.
Cavallini E.
Di Mascio A.
Neri A.
Martelli E.

January 2020

A three-dimensional high-fidelity numerical simulation of a small-scale solid rocket motor is carrie...

Vortex Shedding Inside a Baffled Air Duct

Davis, Philip
Kenny, R. Jeremy

December 2010

Common in the operation of both segmented and un-segmented large solid rocket motors is the occurren...

Parietal vortex shedding as a cause of instability for long solid propellant motors : numerical simulations and comparisons with firing tests

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Parietal vortex shedding as a cause of instability for long solid propellant motors : numerical simulations and comparisons with firing tests

Abstract

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