mohamed Sellam

Documents

Publications

	Bandgap analysis of periodic composite plates considering fluid–structure coupling Runze Zhang , Yu Cong , M. Sellam , Amer Chpoun Journal of Sound and Vibration, 2024, pp.118412. ⟨10.1016/j.jsv.2024.118412⟩ Article dans une revue hal-04518741v1
	Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions Brian Legros , Luc Leger , Azeddine Kourta , Amer Chpoun , Mohamed Sellam Journal of Propulsion and Power, 2023, 39 (6), pp.875-885. ⟨10.2514/1.B39077⟩ Article dans une revue hal-04265352v1
	Experimental investigation of forced flow regime transition in a dual bell nozzle by secondary fluidic injection Luc Léger , Vladeta Zmijanovic , Mohammed Sellam , Amer Chpoun International Journal of Heat and Fluid Flow, 2021, 89, pp.108818. ⟨10.1016/j.ijheatfluidflow.2021.108818⟩ Article dans une revue hal-03233163v1
	Controlled flow regime transition in a dual bell nozzle by secondary radial injection Luc Léger , Vladeta Zmijanovic , Mohammed Sellam , Amer Chpoun Experiments in Fluids, 2020, 61 (12), pp.246. ⟨10.1007/s00348-020-03086-3⟩ Article dans une revue hal-03006165v1
	Effect of Chemical Reactions on the Fluidic Thrust Vectoring of a Plane Nozzle R. Chouicha , Mohammed Sellam , Saïd Bergheul Arabian Journal for Science and Engineering, 2020, 45, pp.7191--7204. ⟨10.1007/s13369-020-04350-8⟩ Article dans une revue hal-02471815v1
	Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle Rachid Chouicha , Mohammed Sellam , Saïd Bergheul Propulsion and Power Research, 2020, ⟨10.1016/j.jppr.2020.04.002⟩ Article dans une revue hal-02970526v1
	Performance improvement of supersonic nozzles design using a high-temperature model Walid Hamaidia , Toufik Zebbiche , Mohamed Sellam , Abderrazak Allali Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, ⟨10.1177/0954410019831862⟩ Article dans une revue hal-02073728v1
	Numerical study of a nonequilibrium H 2 − O 2 rocket nozzle flow Abderrahmane Zidane , Rabah Haoui , Mohamed Sellam , Zineddine Bouyahiaoui International Journal of Hydrogen Energy, 2019, 44 (8), pp.4361--4373. ⟨10.1016/j.ijhydene.2018.12.149⟩ Article dans une revue hal-01987114v1
	Assessment of transition regimes in a dual-bell nozzle and possibility of active fluidic control Vladeta Zmijanovic , Luc Leger , Mohamed Sellam , Amer Chpoun Aerospace Science and Technology, 2018, 82-83, pp.1-8. ⟨10.1016/j.ast.2018.02.003⟩ Article dans une revue hal-01792973v1
	Design and performance evaluation of a dual bell nozzle H. Kbab , Mohamed Sellam , T. Hamitouche, , Said Bergheul , L. Lagab, Acta Astronautica, 2017, 130, pp.52--59. ⟨10.1016/j.actaastro.2016.10.015⟩ Article dans une revue hal-01398298v1
	Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena for a Flexible Overexpanded Rocket Nozzle N. Bekka , M. Sellam , A. Chpoun Shock Waves, 2017, 2017, ⟨10.1007/978-3-319-46213-4_11⟩ Article dans une revue hal-02398155v1
	New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle N. Bekka , M. Sellam , A. Chpoun Shock Waves, 2017, 1, pp.67-70. ⟨10.1007/978-3-319-46213-4_10⟩ Article dans une revue hal-02398153v1
	Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle (Shock Waves, 10.1007/s00193-015-0575-2) Nadir Bekka , Mohamed Sellam , Amer Chpoun Shock Waves, 2016, 26 (4), pp.535--536. ⟨10.1007/s00193-016-0687-3⟩ Article dans une revue hal-01367794v1
	Numerical simulation of reactive flows in overexpanded supersonic nozzle with film cooling Mohamed Sellam , Amer Chpoun International Journal of Aerospace Engineering, 2015, 2015, (elec. proc.). ⟨10.1155/2015/252404⟩ Article dans une revue hal-01176470v1
	Aeroelastic stability analysis of flexible overexpanded rocket nozzle Nadir Bekka , Mohamed Sellam, , Amer Chpoun Shock Waves, 2015, pp.(in Press). ⟨10.1007/s00193-015-0575-2⟩ Article dans une revue hal-01176467v1
	Experimental–Numerical Parametric Investigation of a Rocket Nozzle Secondary Injection Thrust Vectoring V. Zmijanovic , L. Leger , E. Depussay , M. Sellam , Eric Depussay, Journal of Propulsion and Power, 2015, 32 (1), ⟨10.2514/1.B35721⟩ Article dans une revue hal-02398152v1
	Assessment of gas thermodynamic characteristics on fluidic thrust vectoring performance: Analytical, experimental and numerical study Mohamed Sellam, , Vladeta Zmijanović , Luc Léger, , Amer Chpoun International Journal of Heat and Fluid Flow, 2015, 53, pp.156--166. ⟨10.1016/j.ijheatfluidflow.2015.03.005⟩ Article dans une revue hal-01176456v1
	Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration Nadir Bekka , Mohamed Sellam , Amer Chpoun Journal of Fluids and Structures, 2015, 56, pp.89--106. ⟨10.1016/j.jfluidstructs.2015.04.005⟩ Article dans une revue hal-01186406v1
	Thrust shock vector control of an axisymmetric conical supersonic nozzle via secondary transverse gas injection Vladeta Zmijanović , Viviana Lago , Mohamed Sellam, , Amer Chpoun Shock Waves, 2014, 24 (1), pp.97--111. ⟨10.1007/s00193-013-0479-y⟩ Article dans une revue hal-01176489v1
	Numerical investigation of overexpanded nozzle flows: Asymmetrical configuration and hysteresis phenomenon Mohamed Sellam , Guillaume Fournier , Amer Chpoun , Philippe Reijasse Shock Waves, 2014, 24 (1), pp.33--39. ⟨10.1007/s00193-013-0458-3⟩ Article dans une revue hal-01176482v1
	Visualization by discharge illumination technique and modification by plasma actuator of rarefied Mach 2 airflow around a cylinder Luc Léger, , Mohamed Sellam, , Emerson Barbosa , Eric Depussay, Measurement Science and Technology, 2013, 24 (6), pp.065401. ⟨10.1088/0957-0233/24/6/065401⟩ Article dans une revue hal-01172717v1
	Thrust vectoring effects of a transverse gas injection into a supersonic cross-flow of an axisymmetric C-D nozzle V. Zmijanovic , V. Lago , L. Leger , E. Depussay , M. Sellam Advances in Aerospace Sciences (AAS). Progress in Propulsion Physics, 2013, 4, ⟨10.1051/eucass/201304227⟩ Article dans une revue hal-02398151v1
	Fluidic thrust vectoring of an axisymmetrical nozzle: an analytical model Mohamed Sellam , Amer Chpoun , Vladeta Zmijanovic , Viviana Lago International Journal of Aerodynamics, 2012, 2 (2/3/4), pp.193. ⟨10.1504/IJAD.2012.049112⟩ Article dans une revue hal-04421489v1
	Thrust vectoring through fluid injection in an axisymmetrical supersonic nozzle: Theoretical and computational study N. Maarouf , M. Sellam , Michel Grignon , A. Chpoun Shock Waves, 2009, pp.1141-1146. ⟨10.1007/978-3-540-85181-3_56⟩ Article dans une revue hal-04421474v1
	Numerical study of heat transfer around the small scale airfoil using various turbulence models Nadir Bekka , Rachid Bessaïh , Mohamed Sellam , Amer Chpoun Numerical Heat Transfer, Part A Applications, 2009, 56 (12), pp.946--969. ⟨10.1080/10407780903508005⟩ Article dans une revue hal-01179797v1
	Pulsed detonation engine. Numerical study M. Sellam , A. Forestier Journal de Physique IV Proceedings, 2000, 10 (PR11), pp.Pr11-165-Pr11-174. ⟨10.1051/jp4:20001117⟩ Article dans une revue hal-04414427v1

	Potential benefits of radial secondary injection of helium in dual-bell nozzles Brian Legros , Luc Léger , Amer Chpoun , Mohamed Sellam , Azeddine Kourta 57th 3AF International Conference on Applied Aerodynamics, 3AF, Mar 2023, Bordeaux, France Communication dans un congrès hal-04386970v1
	FLUIDIC CONTROL OF FLOW REGIME TRANSITION AND RETRANSITION IN A DUAL-BELL LAUNCHER NOZZLE Brian Legros , Luc Léger , Azeddine Kourta , Abderrahmane Sefir , Mohamed Sellam 8TH EDITION OF THE 3AF SPACE PROPULSION CONFERENCE, 3AF, May 2022, Estoril, Portugal Communication dans un congrès hal-04040496v1
	Enhanced supersonic Annular Nozzle performances: Analysis of flow separation and side loads phenomena Walid Hamaidia , Toufik Yahiaoui , M. Sellam 2nd Global Summit and Expo on Aerospace and Mechanical Engineering (GSEAME2022), Oct 2022, Dubai, United Arab Emirates Communication dans un congrès hal-04529570v1
	An Inverse CFD Modeling Approach for the Identification of Contaminant Source on an Industrial City N. Bekka , P. Kumar , A.A Feiz , S.K. Singh , M. Sellam HARMO 17, May 2016, Budapest, Hungary Communication dans un congrès hal-02416709v1
	Caractérisation d'une Source de Pollution En Milieu Urbain Par Simulation Numérique Directe et Inverse E. Barbosa , A.A. Feiz , P. Kumar , P. Ngae , M. Sellam CAM 2015, Oct 2015, El-Oued, Algeria Communication dans un congrès hal-02416706v1
	Direct Numerical Simulations of the Interaction between an Oblique Shock Wave and a Boundary Layer Developing Along a Flat Plate Guillaume Fournier , Mohamed Sellam , Amer Chpoun , Yann Fraigneau , Christian Tenaud 30th International Symposium on Shock Waves, Springer, Jul 2015, Tel Aviv, Israel Communication dans un congrès hal-01629393v1
	A New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Over-Expanded Roket Nozzle N. Bekka , M. Sellam , A. Chpoun ISSW30, Jul 2015, Tel-Aviv, Israel Communication dans un congrès hal-02416696v1
	Etude de Léffet Thermique Sur Les Performances Aérodynamiques Des Microdrones (MAV) N. Bekka , R. Bessaih , M. Sellam , A. Chpoun CAM 2015, Oct 2015, El Oued, Algeria Communication dans un congrès hal-02416697v1
	Fluid structure interaction phenomena in highly over-expanded rocket nozzle Nadir Bekka , Mohamed Sellam , Grégory Turbelin , Amer Chpoun 11th International Conference of Fluid Dynamics, Dec 2013, Alexandria, Egypt Communication dans un congrès hal-02367721v1
	Estimation du coefficient de poussée pour une tuyère de propulsion Mohamed Sellam , A. Benarous , A. Liazid 21ème Congrès Français de Mécanique (CFM), Aug 2013, Bordeaux, France Communication dans un congrès hal-04441469v1
	Effects of shock Interactions by transverse injection in a fluidically vectored CD nozzle. Vladeta Zmijanovic , Luc Leger , Viviana Lago , Mohamed Sellam , Amer Chpoun 20th International Shock Interaction Symposium (ISIS), Aug 2012, Stockholm, Sweden Communication dans un congrès hal-04440679v1
	Effects of the inlet gases thermodynamic properties on a fluidically thrust vectorized supersonic nozzle Vladeta Zmijanović , Luc Léger, , Viviana Lago , Mohamed Sellam, , Amer Chpoun 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Sep 2012, Tours, France. (elec. proc.) Communication dans un congrès hal-01176565v1
	Experimental and Numerical Study of Thrust-Vectoring Effects by Transverse Gas Injection into a Propulsive Axisymmetric C-D Nozzle Vladeta Zmijanovic , Luc Leger , Viviana Lago , Mohamed Sellam , Amer Chpoun 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sep 2012, Tours (France), France. pp.193, ⟨10.2514/6.2012-3874⟩ Communication dans un congrès hal-04426716v1
	Thrust Shock Vector Control of an Axisymmetric C-D Nozzle via Transverse Gas Injection V. Zmijanovic , V. Lago , S. Palerm , J. Oswald , Mohamed Sellam 28th International Symposium on Shock Waves, Kontis.K, Jul 2012, Manchester (UK), United Kingdom. pp.171-177, ⟨10.1007/978-3-642-25685-1_28⟩ Communication dans un congrès hal-04440607v1
	Secondary injection thrust vectoring of an axisymmetric cd nozzle for small space launchers & vehicles Vladeta Zmijanović , Sandrine Palerm , Mohamed Sellam, , Amer Chpoun 63rd International Astronautical Congress 2012 (IAC 2012), Oct 2012, Naples, Italy. pp.7457--7468 Communication dans un congrès hal-01176502v1
	Fluid-Structure interaction for a flexible over expanded rocket nozzle using the aeroelastic stability model Nadir Bekka , Mohamed Sellam , Grégory Turbelin , Amer Chpoun ISSW 28, Jul 2011, Manchester, United Kingdom Communication dans un congrès hal-02367714v1
	Numerical Investigation of Over-Expanded Nozzle Flows: Influence of Internal Shock Waves G. Fournier , A. Chpoun , Mohamed Sellam , Ph. Rijasse , S. Girard ISSW 28, Jul 2011, Manchester (UK), United Kingdom. pp.147-152, ⟨10.1007/978-3-642-25685-1_24⟩ Communication dans un congrès hal-04440592v1
	Numerical Investigation of Over-Expanded Nozzle Flows: Influence of Internal Shock Waves Guillaume Fournier , Amer Chpoun , Mohamed Sellam , Philippe Reijasse , Sébastien Girard 28th International Symposium on Shock Waves, Jul 2011, Manchester (UK), United Kingdom. pp.147-152, ⟨10.1007/978-3-642-25685-1_24⟩ Communication dans un congrès hal-04441773v1
	Computational and modelling study of fluid injection for thrust vectoring in an axisymmetric supersonic nozzle N. Maarouf , M. Sellam , Michel Grignon , A. Chpoun 18th International Shock Interaction Symposium, Jul 2008, Rouen, France Communication dans un congrès hal-04442435v1
	Transitional shock wave boundary layer interaction in hypersonic flow Atmospheric Re-entry Vehicles and systems L. Vandomme , B. Chanetz , R. Benay , B. Louis , A. Chpoun Symposium AAAF, Mar 2003, Arcachon (France), France Communication dans un congrès hal-04442376v1
	Étude numérique et expérimentale de la structure de l'écoulement autour d'une sphère placée dans un écoulement raréfié Mohamed Sellam , A. Lebehot , Viviana Lago , Amer Chpoun , Michel Dudeck 7ème Congrès de la SFP sur les plasmas (SFP Plasmas 2001, Mar 2001, La Baule, France Communication dans un congrès hal-04441442v1
	Pulsed detonation engine M. Sellam , A. Forestier , G. Poissant IVth International Workshop on Ram Accelerator (RAMAC IV), Sep 1999, Poitiers, France Communication dans un congrès hal-04442402v1

	SYSTEM FOR CONTROLLING SPEED TRANSITION AND THRUST VECTORISATION IN A MULTIPLE-SHAPED NOZZLE BY SECONDARY INJECTION Mohamed Sellam , Amer Chpoun , Luc Leger , Vladeta Zmijanovic Japan, Patent n° : 7273059. 2023 Brevet hal-04439091v1
	SYSTEM FOR CONTROLLING SPEED TRANSITION AND THRUST VECTORISATION IN A MULTIPLE-SHAPED NOZZLE BY SECONDARY INJECTION M. Sellam , Amer Chpoun , Luc Leger , Vladeta Zmijanovic United States, Patent n° : US 11,661,910B2. 2023 Brevet hal-04415223v1

	Synthèse des travaux de recherche dans le domaine des écoulements supersoniques centrés sur les problématiques des tuyères propulsives Mohamed Sellam Mécanique des fluides [physics.class-ph]. Université Evry -Val d'Essonne, 2013 HDR tel-04415470v1

	Numerical investigation of downstream flow parameters influence on Mach stem size M. Sellam , A Chpoun Shock Waves, 2005, pp.399-404 Autre publication scientifique hal-04421542v1

	Secondary Injectant Gas Thermodynamic Properties Effects on Fluidic Thrust Vectoring Performances of a Supersonic Nozzle A. Chpoun , M. Sellam , V. Zmijanovic , L. Léger 30th International Symposium on Shock Waves, 1, Springer; Springer International Publishing, pp.539-543, 2017, ⟨10.1007/978-3-319-46213-4_92⟩ Proceedings/Recueil des communications hal-02398154v1
	Design and performances of the dual-bell nozzle Hamitouche Toufik , Mohamed Sellam , Kbab Hakim , Bergheul Said , Lagab Lynda 2016 IEEE Aerospace Conference, IEEE, pp.1-7, 2016, ⟨10.1109/AERO.2016.7500518⟩ Proceedings/Recueil des communications hal-04421431v1
	Characterization of Strong Detonation Waves in Nitromethane M. Sellam , H.N Presles , C Brochet , R Cheret International Symposium on Detonation (8th), Office of Naval Research (ONR), pp.425-430, 1985 Proceedings/Recueil des communications hal-04421532v1

	Calculation of Overdriven Detonation In Nitromethane K. Tanaka , S. Fujiwara , M. Sellam , H.N Presles , C. Brochet Elsevier Sciences Publishers. Shock Waves in Condensed Matter, S.C.Schmidt, N.C. Holmes, pp.515-518, 1987 Chapitre d'ouvrage hal-04421515v1

mohamed Sellam

Publications

Bandgap analysis of periodic composite plates considering fluid–structure coupling

Parametrical Investigation of Transverse Injection in a Dual-Bell Nozzle During Altitude-Varying Conditions

Experimental investigation of forced flow regime transition in a dual bell nozzle by secondary fluidic injection

Controlled flow regime transition in a dual bell nozzle by secondary radial injection

Effect of Chemical Reactions on the Fluidic Thrust Vectoring of a Plane Nozzle

Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle

Performance improvement of supersonic nozzles design using a high-temperature model

Numerical study of a nonequilibrium H 2 − O 2 rocket nozzle flow

Assessment of transition regimes in a dual-bell nozzle and possibility of active fluidic control

Design and performance evaluation of a dual bell nozzle

Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena for a Flexible Overexpanded Rocket Nozzle

New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle

Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle (Shock Waves, 10.1007/s00193-015-0575-2)

Numerical simulation of reactive flows in overexpanded supersonic nozzle with film cooling

Aeroelastic stability analysis of flexible overexpanded rocket nozzle

Experimental–Numerical Parametric Investigation of a Rocket Nozzle Secondary Injection Thrust Vectoring

Assessment of gas thermodynamic characteristics on fluidic thrust vectoring performance: Analytical, experimental and numerical study

Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration

Thrust shock vector control of an axisymmetric conical supersonic nozzle via secondary transverse gas injection

Numerical investigation of overexpanded nozzle flows: Asymmetrical configuration and hysteresis phenomenon

Visualization by discharge illumination technique and modification by plasma actuator of rarefied Mach 2 airflow around a cylinder

Thrust vectoring effects of a transverse gas injection into a supersonic cross-flow of an axisymmetric C-D nozzle

Fluidic thrust vectoring of an axisymmetrical nozzle: an analytical model

Thrust vectoring through fluid injection in an axisymmetrical supersonic nozzle: Theoretical and computational study

Numerical study of heat transfer around the small scale airfoil using various turbulence models

Pulsed detonation engine. Numerical study

Potential benefits of radial secondary injection of helium in dual-bell nozzles

FLUIDIC CONTROL OF FLOW REGIME TRANSITION AND RETRANSITION IN A DUAL-BELL LAUNCHER NOZZLE

Enhanced supersonic Annular Nozzle performances: Analysis of flow separation and side loads phenomena

An Inverse CFD Modeling Approach for the Identification of Contaminant Source on an Industrial City

Caractérisation d'une Source de Pollution En Milieu Urbain Par Simulation Numérique Directe et Inverse

Direct Numerical Simulations of the Interaction between an Oblique Shock Wave and a Boundary Layer Developing Along a Flat Plate

A New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Over-Expanded Roket Nozzle

Etude de Léffet Thermique Sur Les Performances Aérodynamiques Des Microdrones (MAV)

Fluid structure interaction phenomena in highly over-expanded rocket nozzle

Estimation du coefficient de poussée pour une tuyère de propulsion

Effects of shock Interactions by transverse injection in a fluidically vectored CD nozzle.

Effects of the inlet gases thermodynamic properties on a fluidically thrust vectorized supersonic nozzle

Experimental and Numerical Study of Thrust-Vectoring Effects by Transverse Gas Injection into a Propulsive Axisymmetric C-D Nozzle

Thrust Shock Vector Control of an Axisymmetric C-D Nozzle via Transverse Gas Injection

Secondary injection thrust vectoring of an axisymmetric cd nozzle for small space launchers & vehicles

Fluid-Structure interaction for a flexible over expanded rocket nozzle using the aeroelastic stability model

Numerical Investigation of Over-Expanded Nozzle Flows: Influence of Internal Shock Waves

Numerical Investigation of Over-Expanded Nozzle Flows: Influence of Internal Shock Waves

Computational and modelling study of fluid injection for thrust vectoring in an axisymmetric supersonic nozzle

Transitional shock wave boundary layer interaction in hypersonic flow Atmospheric Re-entry Vehicles and systems

Étude numérique et expérimentale de la structure de l'écoulement autour d'une sphère placée dans un écoulement raréfié

Pulsed detonation engine

SYSTEM FOR CONTROLLING SPEED TRANSITION AND THRUST VECTORISATION IN A MULTIPLE-SHAPED NOZZLE BY SECONDARY INJECTION

SYSTEM FOR CONTROLLING SPEED TRANSITION AND THRUST VECTORISATION IN A MULTIPLE-SHAPED NOZZLE BY SECONDARY INJECTION

Synthèse des travaux de recherche dans le domaine des écoulements supersoniques centrés sur les problématiques des tuyères propulsives

Numerical investigation of downstream flow parameters influence on Mach stem size

Secondary Injectant Gas Thermodynamic Properties Effects on Fluidic Thrust Vectoring Performances of a Supersonic Nozzle

Design and performances of the dual-bell nozzle

Characterization of Strong Detonation Waves in Nitromethane

Calculation of Overdriven Detonation In Nitromethane