المؤلفون: Sidali HAIF, Hakim KBAB, Amina BENKHEDDA

المصدر: INCAS Bulletin, Vol 15, Iss 2, Pp 33-47 (2023)

مصطلحات موضوعية: e-d nozzle, dual bell nozzle, ansys-fluent, method of characteristics (moc), fortran, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://bulletin.incas.ro/files/haif_kbab__benkhedda__vol_15_iss_2.pdf; https://doaj.org/toc/2066-8201; https://doaj.org/toc/2247-4528

URL الوصول: https://doaj.org/article/c17cd5aba76b4c2babfc3c98279b3f2c

المؤلفون: Legros, Brian, Léger, Luc, Chpoun, Amer, Sellam, Mohamed, Kourta, Azeddine

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes - CNRS Ingénierie (INSIS - CNRS), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE)-Université Paris-Saclay, Laboratoire pluridisciplinaire de recherche en ingénierie des systèmes, mécanique et énergétique (PRISME), Université d'Orléans (UO)-Institut National des Sciences Appliquées - Centre Val de Loire (INSA CVL), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA), 3AF, ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011)

المصدر: 57th 3AF International Conference on Applied Aerodynamics
https://hal.science/hal-04386970
57th 3AF International Conference on Applied Aerodynamics, 3AF, Mar 2023, Bordeaux, France

مصطلحات موضوعية: Shock wave, Rocket nozzle, Dual-bell nozzle, Dual-bell nozzle rocket nozzle flow control, Secondary injection, Active flow control, Transition regime, Tuyère à double galbe, [PHYS.MECA.MEFL]Physics [physics]/Mechanics [physics]/Fluid mechanics [physics.class-ph]

جغرافية الموضوع: Bordeaux, France

Relation: hal-04386970; https://hal.science/hal-04386970; https://hal.science/hal-04386970/document; https://hal.science/hal-04386970/file/Conference_Bordeaux_2023_HAL_VERSION.pdf

الاتاحة: https://hal.science/hal-04386970
https://hal.science/hal-04386970/document
https://hal.science/hal-04386970/file/Conference_Bordeaux_2023_HAL_VERSION.pdf

المؤلفون: Legros, Brian, Léger, Luc, Kourta, Azeddine, Sefir, Abderrahmane, Sellam, Mohamed, Chpoun, Amer

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes - CNRS Ingénierie (INSIS - CNRS), Laboratoire pluridisciplinaire de recherche en ingénierie des systèmes, mécanique et énergétique (PRISME), Université d'Orléans (UO)-Institut National des Sciences Appliquées - Centre Val de Loire (INSA CVL), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE)-Université Paris-Saclay, 3AF, ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011)

المصدر: 8TH EDITION OF THE 3AF SPACE PROPULSION CONFERENCE
https://hal.science/hal-04040496
8TH EDITION OF THE 3AF SPACE PROPULSION CONFERENCE, 3AF, May 2022, Estoril, Portugal

مصطلحات موضوعية: dual-bell nozzle rocket nozzle flow control, dual-bell nozzle, rocket nozzle, flow control, [SPI.FLUID]Engineering Sciences [physics]/Reactive fluid environment

جغرافية الموضوع: Estoril, Portugal

Time: Estoril, Portugal

Relation: hal-04040496; https://hal.science/hal-04040496; https://hal.science/hal-04040496/document; https://hal.science/hal-04040496/file/SP2022_378_LEGROS.pdf

الاتاحة: https://hal.science/hal-04040496
https://hal.science/hal-04040496/document
https://hal.science/hal-04040496/file/SP2022_378_LEGROS.pdf

المؤلفون: Legros, Brian, Leger, Luc, Kourta, Azeddine, Chpoun, Amer, Sellam, Mohamed

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes - CNRS Ingénierie (INSIS - CNRS), Laboratoire pluridisciplinaire de recherche en ingénierie des systèmes, mécanique et énergétique (PRISME), Université d'Orléans (UO)-Institut National des Sciences Appliquées - Centre Val de Loire (INSA CVL), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE)-Université Paris-Saclay, Grant No. ANR-11-LABX-0006-01 of the Investissements d’Avenir LabEx CAPRYSSES, ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011)

المصدر: ISSN: 0748-4658.

مصطلحات موضوعية: Dual-bell nozzle, Active flow control, Rocket nozzles, Shock wave, Wind tunnel, Aerodynamic, Boundary layer control, Propulsion, [PHYS.MECA.MEFL]Physics [physics]/Mechanics [physics]/Fluid mechanics [physics.class-ph], [SPI.FLUID]Engineering Sciences [physics]/Reactive fluid environment

Relation: hal-04265352; https://hal.science/hal-04265352; https://hal.science/hal-04265352/document; https://hal.science/hal-04265352/file/LegrosJPP_reviewed.pdf

الاتاحة: https://hal.science/hal-04265352
https://hal.science/hal-04265352/document
https://hal.science/hal-04265352/file/LegrosJPP_reviewed.pdf
https://doi.org/10.2514/1.B39077

المؤلفون: Andrea Ferrero, Antonietta Conte, Emanuele Martelli, Francesco Nasuti, Dario Pastrone

المساهمون: Ferrero, Andrea, Conte, Antonietta, Martelli, Emanuele, Nasuti, Francesco, Pastrone, Dario

مصطلحات موضوعية: dual-bell nozzle, side load, fluidic control, trajectory optimisation

Relation: info:eu-repo/semantics/altIdentifier/wos/WOS:000772023900011; volume:193; firstpage:130; lastpage:137; numberofpages:8; journal:ACTA ASTRONAUTICA; https://hdl.handle.net/11573/1683882; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85122917535

الاتاحة: https://hdl.handle.net/11573/1683882
https://doi.org/10.1016/j.actaastro.2021.12.048

المؤلفون: Cimini M., Martelli E., Bernardini M.

المساهمون: Cimini, M., Martelli, E., Bernardini, M.

مصطلحات موضوعية: dual-bell nozzle, flow separation, hybrid RANS/LES, passive control, side loads

Relation: info:eu-repo/semantics/altIdentifier/wos/WOS:000612603800001; numberofpages:24; journal:FLOW TURBULENCE AND COMBUSTION; http://hdl.handle.net/11573/1496699; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85099986189

الاتاحة: http://hdl.handle.net/11573/1496699
https://doi.org/10.1007/s10494-021-00243-4

المؤلفون: Léger, Luc, Zmijanovic, Vladeta, Sellam, Mohammed, Chpoun, Amer

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes - CNRS Ingénierie (INSIS - CNRS), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE)-Université Paris-Saclay, ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011)

المصدر: ISSN: 0142-727X ; International Journal of Heat and Fluid Flow ; https://hal.science/hal-03233163 ; International Journal of Heat and Fluid Flow, 2021, 89, pp.108818. ⟨10.1016/j.ijheatfluidflow.2021.108818⟩.

مصطلحات موضوعية: Dual bell nozzle, Flow control, Nozzle flow, Supersonic flow, Transition regime, [SPI.MECA]Engineering Sciences [physics]/Mechanics [physics.med-ph]

Relation: hal-03233163; https://hal.science/hal-03233163; https://hal.science/hal-03233163/document; https://hal.science/hal-03233163/file/S0142727X21000485.pdf; PII: S0142-727X(21)00048-5

الاتاحة: https://hal.science/hal-03233163
https://hal.science/hal-03233163/document
https://hal.science/hal-03233163/file/S0142727X21000485.pdf
https://doi.org/10.1016/j.ijheatfluidflow.2021.108818

المؤلفون: Legros, Brian

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes - CNRS Ingénierie (INSIS - CNRS), Laboratoire pluridisciplinaire de recherche en ingénierie des systèmes, mécanique et énergétique (PRISME), Université d'Orléans (UO)-Institut National des Sciences Appliquées - Centre Val de Loire (INSA CVL), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA), Université d'Orléans, Azeddine Kourta, Luc Léger, ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011)

المصدر: https://theses.hal.science/tel-04588641 ; Mechanical engineering [physics.class-ph]. Université d'Orléans, 2024. English. ⟨NNT : 2024ORLE1008⟩.

مصطلحات موضوعية: Active flow control, Dual-Bell nozzle, Contrôle actif d'écoulement, Tuyère à double galbe, [SPI.MECA.GEME]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanical engineering [physics.class-ph]

Relation: NNT: 2024ORLE1008

الاتاحة: https://theses.hal.science/tel-04588641
https://theses.hal.science/tel-04588641v1/document
https://theses.hal.science/tel-04588641v1/file/2024ORLE1008_va.pdf

المؤلفون: Kazuhiko YOKOTA, Yuki KOYAGI, 小八木 裕貴, 横田 和彦

المصدر: The Proceedings of the Fluids engineering conference. 2022, :OS03-40

المؤلفون: Antonietta Conte, Andrea Ferrero, Francesco Larocca, Dario Pastrone

المساهمون: Conte, Antonietta, Ferrero, Andrea, Larocca, Francesco, Pastrone, Dario Giuseppe

مصطلحات موضوعية: rocket nozzle, dual-bell, CFD, shock capturing

وصف الملف: ELETTRONICO

Relation: info:eu-repo/semantics/altIdentifier/isbn/978-1-62410-590-6; ispartofbook:Titolo volume non avvalorato; AIAA Propulsion and Energy 2019 Forum; numberofpages:10; http://hdl.handle.net/11583/2750894; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85095972484

الاتاحة: http://hdl.handle.net/11583/2750894
https://doi.org/10.2514/6.2019-4115
https://arc.aiaa.org/doi/10.2514/6.2019-4115

المؤلفون: Stark, Ralf, Kallina, Philipp Johannes, General, Stephan, Schneider, Dirk

مصطلحات موضوعية: film-cooling, dual-bell nozzle, rocket propulsion

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::0c0378a22e7a26f49a5f65611ec24b4f
https://elib.dlr.de/192629/

المؤلفون: Conte, Antonietta

مصطلحات موضوعية: high-vacuum environments, acoustic igniter, fluidic control, rocket engines, rocket engine nozzles, sonic nozzle, dual-bell nozzle, overexpanded flow, underexpanded flow, high-vacuum plume test facility, CFD, DSMC, Settore ING-IND/07 - Propulsione Aerospaziale

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______2153::7a77481f402a2c1fec5d84baea20e441
http://hdl.handle.net/11583/2962963

المؤلفون: Andrea Ferrero, Francesco Nasuti, Antonietta Conte, Emanuele Martelli, Dario Giuseppe Pastrone

المساهمون: AIAA Propulsion and Energy Forum, Ferrero, A., Conte, A., Martelli, E., Nasuti, F., Pastrone, D.

المصدر: AIAA Propulsion and Energy 2021 Forum.

مصطلحات موضوعية: Fluidic control, Materials science, Dual-bell nozzle, Space launcher, Dual-bell transition, Fluidics, Bell nozzle, Mechanics, Space (mathematics), Dual (category theory)

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::10d6f43975698d05735fdf730b25b7bb
https://doi.org/10.2514/6.2021-3586

المؤلفون: Abadie Ardon, Manuel R

المصدر: Honors College Theses

مصطلحات موضوعية: rocket nozzles CFD aerospike Dual-Bell Expansion-Deflection, Aerodynamics and Fluid Mechanics, Propulsion and Power

وصف الملف: application/pdf

Relation: https://digitalcommons.georgiasouthern.edu/honors-theses/747; https://digitalcommons.georgiasouthern.edu/context/honors-theses/article/1825/viewcontent/Abadie_Thesis_Final.pdf

الاتاحة: https://digitalcommons.georgiasouthern.edu/honors-theses/747
https://digitalcommons.georgiasouthern.edu/context/honors-theses/article/1825/viewcontent/Abadie_Thesis_Final.pdf

المؤلفون: Emanuele Martelli, Matteo Bernardini, Matteo Cimini

المساهمون: Cimini, M., Martelli, E., Bernardini, M.

مصطلحات موضوعية: General Chemical Engineering, Nozzle, Rocket engine nozzle, General Physics and Astronomy, 02 engineering and technology, 01 natural sciences, 010305 fluids & plasmas, Dual-bell nozzle, Flow separation, Passive control, Side loads, Hybrid RANS/LES, Physics::Fluid Dynamics, Flow separation, symbols.namesake, 0203 mechanical engineering, hybrid RANS/LES, 0103 physical sciences, Physical and Theoretical Chemistry, side loads, passive control, Physics, 020301 aerospace & aeronautics, Shock (fluid dynamics), Turbulence, Reynolds number, Mechanics, dual-bell nozzle, flow separation, Inflection point, symbols, Detached eddy simulation

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b3cb38a57b5d2ab88801fbefc55b1449
http://hdl.handle.net/11591/442803

المؤلفون: Michael Oschwald, Konstantin Kostyrkin, Ralf Stark, Dirk Schneider, Chloé Génin

المصدر: Journal of Propulsion and Power. 36:47-58

مصطلحات موضوعية: Propellant, Materials science, Mechanical Engineering, Nozzle, nozzle flow, Mathematics::Analysis of PDEs, film cooling, Aerospace Engineering, Mechanics, Regenerative cooling (rocket), Boundary layer thickness, dual bell nozzle, Physics::Fluid Dynamics, Hysteresis, Fuel Technology, Space and Planetary Science, Bell nozzle, Combustion chamber, Reynolds-averaged Navier–Stokes equations

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4c59550891341cb2b62036be5a0061a5
https://doi.org/10.2514/1.b37299

المؤلفون: Donghyuk KANG, Hiroyoshi YAMAGUCHI, Kazuhiko YOKOTA, Kouichi YONEZAWA, Ryo ANDO, 姜 東赫, 安藤 諒, 山口 裕理, 横田 和彦, 米澤 宏一

المصدر: The Proceedings of Conference of Kanto Branch. 2018, :0504

المؤلفون: Hiroyoshi YAMAGUCHI, Kazuhiko YOKOTA, Koichi YONEZAWA, Wakana TSURU, 山口 裕理, 横田 和彦, 米澤 宏一, 鶴 若菜

المصدر: The Proceedings of Conference of Hokkaido Branch. 2018, :131

المؤلفون: Abhilash Narayan, S. Panneerselvam

مصطلحات موضوعية: Altitude adaptation, Dual bell nozzle, Nozzle pressure ratio, Over-expansion factor

Relation: https://zenodo.org/communities/waset; https://doi.org/10.5281/zenodo.1062505; https://doi.org/10.5281/zenodo.1062506; oai:zenodo.org:1062506

الاتاحة: https://doi.org/10.5281/zenodo.1062506

المؤلفون: Mohamed Sellam, Amer Chpoun, Luc Leger, Vladeta Zmijanovic

المساهمون: Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes (INSIS), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE), ANR-11-LABX-0006,CAPRYSSES,Cinétique chimique et Aérothermodynamique pour des Propulsions et des Systèmes Energétiques Propres(2011), Université d'Orléans (UO)-Centre National de la Recherche Scientifique (CNRS)-Institut des Sciences de l'Ingénierie et des Systèmes (INSIS - CNRS)

المصدر: Aerospace Science and Technology
Aerospace Science and Technology, Elsevier, 2018, 82-83, pp.1-8. ⟨10.1016/j.ast.2018.02.003⟩
Aerospace Science and Technology, 2018, 82-83, pp.1-8. ⟨10.1016/j.ast.2018.02.003⟩

مصطلحات موضوعية: 020301 aerospace & aeronautics, Materials science, Secondary fluidic injection, Hysteresis, Nozzle, Rotational symmetry, Aerospace Engineering, 02 engineering and technology, Mechanics, [SPI.MECA]Engineering Sciences [physics]/Mechanics [physics.med-ph], 01 natural sciences, 010305 fluids & plasmas, Dual (category theory), Physics::Fluid Dynamics, Altitude compensating nozzle, Dual-bell nozzle, 0203 mechanical engineering, Transition, Flow regimes, 0103 physical sciences, Fluidics, Active flow control, Bell nozzle, Envelope (mathematics)

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f1c6d38b8503a99ac03a521a060e5bb3
https://doi.org/10.1016/j.ast.2018.02.003