المؤلفون: J. Hassan, R. Marsilio, G. M. Di Cicca, M. Ferlauto

المساهمون: Hassan, J., Marsilio, R., Di Cicca, G. M., Ferlauto, M.

مصطلحات موضوعية: Aerospike, rocket Nozzle, Differential Throttling, Thrust Vectoring

Relation: ispartofbook:ICAS PROCEEDINGS 2024; 34th Congress of the International Council of the Aeronautical Sciences; numberofpages:9; https://hdl.handle.net/11583/2993321; https://www.icas.org/ICAS_ARCHIVE/ICAS2024/data/papers/ICAS2024_0944_paper.pdf

الاتاحة: https://hdl.handle.net/11583/2993321
https://www.icas.org/ICAS_ARCHIVE/ICAS2024/data/papers/ICAS2024_0944_paper.pdf

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: Emanuele Resta, Gaetano Maria Di Cicca, Michele Ferlauto, Roberto Marsilio

المساهمون: Resta, Emanuele, DI CICCA, GAETANO MARIA, Ferlauto, Michele, Marsilio, Roberto

مصطلحات موضوعية: Aerospike, Advanced Nozzle, Rocket Nozzle, Experimental testing supersonic flows

وصف الملف: ELETTRONICO

Relation: ispartofbook:Aeronautics and Astronautics - AIDAA XXVII International Congress; AIDAA 2023; firstpage:675; lastpage:678; numberofpages:4; serie:MATERIALS RESEARCH PROCEEDINGS; https://hdl.handle.net/11583/2983177; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85185767198; https://doi.org/10.21741/9781644902813-145

الاتاحة: https://hdl.handle.net/11583/2983177
https://doi.org/10.21741/9781644902813-145

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: Airoldi, Alessandro, Boiocchi, Matteo, Natali, Maurizio, Mirani, Chiara, Di Pancrazio, Luca, Consiglio, Gabriele, Ballarin, Pietro, Riva, Marco

المساهمون: Airoldi, Alessandro, Boiocchi, Matteo, Natali, Maurizio, Mirani, Chiara, Di Pancrazio, Luca, Consiglio, Gabriele, Ballarin, Pietro, Riva, Marco

مصطلحات موضوعية: Composites, Corrugated laminates, Manufacturing, Morphing, Rocket nozzle, Thrust vector control

Relation: info:eu-repo/semantics/altIdentifier/wos/WOS:000895012100002; volume:30; firstpage:399; lastpage:429; numberofpages:31; journal:APPLIED COMPOSITE MATERIALS; https://hdl.handle.net/11311/1226031; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85143623819; https://doi.org/10.1007/s10443-022-10082-9

الاتاحة: https://hdl.handle.net/11311/1226031
https://doi.org/10.1007/s10443-022-10082-9

المؤلفون: Nithin Somasekharan, A. R. Srikrishnan, Harihara Sudhan Kumar, Krishna Prasad Ganesh, Akram Mohammad, Ratna Kishore Velamati

المصدر: Entropy; Volume 25; Issue 3; Pages: 481

مصطلحات موضوعية: rocket nozzle cooling, mixing layer studies, diffuser-type coolant injector, film cooling

وصف الملف: application/pdf

Relation: Thermodynamics; https://dx.doi.org/10.3390/e25030481

الاتاحة: https://doi.org/10.3390/e25030481

المؤلفون: Yizhe Chen, Shilong Zhao, Hui Wang, Jun Li, Lin Hua

المصدر: Materials; Volume 16; Issue 4; Pages: 1680

مصطلحات موضوعية: rocket nozzle, tube upsetting-bulging, plastic deformation, critical pressure

وصف الملف: application/pdf

Relation: Metals and Alloys; https://dx.doi.org/10.3390/ma16041680

الاتاحة: https://doi.org/10.3390/ma16041680

المؤلفون: Guelailia, Ahmed, Khorsi, Azzeddine, Boudjemai, Abdelmadjid, Wang, Jin

المصدر: International Journal of Heat and Technology. 36(3):1070-1074

مصطلحات موضوعية: Computational fluid dynamics, Film cooling, Heat, Mass transfer, Propulsion, Rocket nozzle, Thermal protection, Teknik, Maskinteknik, Strömningsmekanik och akustik, Engineering and Technology, Mechanical Engineering, Fluid Mechanics and Acoustics

URL الوصول: https://lup.lub.lu.se/record/1a08e1cb-d5ba-4a2a-9b2d-0c26d9f531bd
http://dx.doi.org/10.18280/ijht.360338

المؤلفون: Roberto Marsilio, Emanuele Resta, Gaetano Di Cicca, Michele Ferlauto

المساهمون: Marsilio, Roberto, Resta, Emanuele, DI CICCA, GAETANO MARIA, Ferlauto, Michele

مصطلحات موضوعية: thrust vectoring, rocket nozzle, active flow control, supersonic nozzle

وصف الملف: ELETTRONICO

Relation: ispartofbook:AIAA SCITECH 2024 Forum; AIAA SCITECH 2024 Forum; numberofpages:10; https://hdl.handle.net/11583/2984988; https://doi.org/10.2514/6.2024-1617

الاتاحة: https://hdl.handle.net/11583/2984988
https://doi.org/10.2514/6.2024-1617

المؤلفون: Gandge, Amar, Basawaraj, Hampali, Chennabasappa

المصدر: Journal of Mines, Metals and Fuels; Volume 69, Issue 12A, December 2021; 234-239 ; 0022-2755

مصطلحات موضوعية: CFD, supersonic rocket nozzle, shockwave, divergent angle

وصف الملف: application/pdf

Relation: https://www.informaticsjournals.com/index.php/jmmf/article/view/30109/21037; https://www.informaticsjournals.com/index.php/jmmf/article/view/30109

الاتاحة: https://www.informaticsjournals.com/index.php/jmmf/article/view/30109
https://doi.org/10.18311/jmmf/2021/30109

المؤلفون: Robayo-Salazar, Rafael, Portocarrero-Hermann, Julián, Díaz-Padrón, Ubaldo, Patiño-Castrillón, Oscar

المصدر: Revista Facultad de Ingeniería; Vol. 29 No. 54 (2020): Continuos Publication; e10662 ; Revista Facultad de Ingeniería; Vol. 29 Núm. 54 (2020): Publicación Continua; e10662 ; 2357-5328 ; 0121-1129

مصطلحات موضوعية: ablative materials, composite materials, propulsion components, rocket engine, rocket nozzle, thermal protection systems, materiales compuestos, materiales ablativos, sistemas de protección térmica, motor cohete, componentes de propulsión, tobera

وصف الملف: application/pdf; application/xml

Relation: https://revistas.uptc.edu.co/index.php/ingenieria/article/view/10662/9330; https://revistas.uptc.edu.co/index.php/ingenieria/article/view/10662/9506; https://revistas.uptc.edu.co/index.php/ingenieria/article/view/10662; https://repositorio.uptc.edu.co/handle/001/14267

الاتاحة: https://repositorio.uptc.edu.co/handle/001/14267
https://revistas.uptc.edu.co/index.php/ingenieria/article/view/10662
https://doi.org/10.19053/01211129.v29.n54.2020.10662

المؤلفون: Yashwanth Bharath, K., Praveen, J., Akash, E., Arravind, R.

المصدر: International Journal of Recent Advances in Multidisciplinary Topics; Vol. 2 No. 6 (2021); 185-186 ; 2582-7839

مصطلحات موضوعية: bell shaped rocket nozzle, Aerospike nozzle, second law of thermodynamics

وصف الملف: application/pdf

Relation: https://journals.ijramt.com/index.php/ijramt/article/view/900/869; https://journals.ijramt.com/index.php/ijramt/article/view/900

الاتاحة: https://journals.ijramt.com/index.php/ijramt/article/view/900

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: Resta, Emanuele, Marsilio, Roberto, Ferlauto, Michele

المساهمون: Resta, Emanuele, Marsilio, Roberto, Ferlauto, Michele

مصطلحات موضوعية: rocket nozzle, aerospace propulsion, hot flow, computational fluid dynamics

وصف الملف: ELETTRONICO

Relation: info:eu-repo/semantics/altIdentifier/isbn/978-1-62410-699-6; ispartofbook:AIAA SCITECH 2023 Forum; AIAA SCITECH 2023 Forum; numberofpages:12; https://hdl.handle.net/11583/2975042; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85198614718

الاتاحة: https://hdl.handle.net/11583/2975042
https://doi.org/10.2514/6.2023-0714
https://arc.aiaa.org/doi/10.2514/6.2023-0714

المؤلفون: Shi Chenhong, Yang Jinpeng, Xu Zhishu

المصدر: MATEC Web of Conferences, Vol 309, p 04008 (2020)

مصطلحات موضوعية: auto disturbance rejection control technology, non-linear load, rocket nozzle, thrust vector control, Engineering (General). Civil engineering (General), TA1-2040

Relation: https://www.matec-conferences.org/articles/matecconf/pdf/2020/05/matecconf_cscns2020_04008.pdf; https://doaj.org/toc/2261-236X; https://doaj.org/article/13dd4bcd60b7438ea46da4513c465db9

الاتاحة: https://doi.org/10.1051/matecconf/202030904008
https://doaj.org/article/13dd4bcd60b7438ea46da4513c465db9

المؤلفون: Di Martino Giuseppe D., Mungiguerra Stefano, Cecere Anselmo, Savino Raffaele, Vinci Antonio, Zoli Luca, Sciti Diletta

مصطلحات موضوعية: ultra-high temperature, ceramic matrix composites, hybrid rocket nozzle, near-zero erosion, computational fluid dynamic simulation

Relation: https://zenodo.org/communities/eu; https://doi.org/10.5281/zenodo.1473368; https://doi.org/10.5281/zenodo.1473369; oai:zenodo.org:1473369

الاتاحة: https://doi.org/10.5281/zenodo.1473369

المؤلفون: Fridh, Jens, Östlund, Jan

مصطلحات موضوعية: methane, rocket nozzle, cooling channel, conjugated heat transfer, Aerospace Engineering, Rymd- och flygteknik

وصف الملف: application/pdf

الاتاحة: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-294136

المؤلفون: Hiroshi SUDA, Kazuhiko YOKOTA, Wakana TSURU, Yuki KOYAGI, 小八木 裕貴, 横田 和彦, 須田 広志, 鶴 若菜

المصدر: The Proceedings of Conference of Kanto Branch. 2021, :11

المؤلفون: Anshul Suri, Ankit Bansal

المصدر: ICTEA: International Conference on Thermal Engineering; Vol. 1 No. 1 (2019): ICTEA ; 2562-9034

مصطلحات موضوعية: Ablative material, modeling, rocket nozzle

وصف الملف: application/pdf

Relation: https://journals.library.torontomu.ca/index.php/ictea/article/view/1197/1204; https://journals.library.torontomu.ca/index.php/ictea/article/view/1197

الاتاحة: https://journals.library.torontomu.ca/index.php/ictea/article/view/1197