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

المصدر: Fluids, Vol 9, Iss 8, p 179 (2024)

مصطلحات موضوعية: aerospike, supersonic nozzles, experimental testing, rocket nozzles, Thermodynamics, QC310.15-319, Descriptive and experimental mechanics, QC120-168.85

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2311-5521/9/8/179; https://doaj.org/toc/2311-5521

URL الوصول: https://doaj.org/article/a075e1170c1141cfabbb4465304d190b

المؤلفون: Marek Pátý, Michael Valášek, Emanuele Resta, Roberto Marsilio, Michele Ferlauto

المصدر: Fluids, Vol 9, Iss 6, p 131 (2024)

مصطلحات موضوعية: passive flow control, vortex identification, residual vorticity, bluff body wake, geometry optimization, Thermodynamics, QC310.15-319, Descriptive and experimental mechanics, QC120-168.85

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2311-5521/9/6/131; https://doaj.org/toc/2311-5521

URL الوصول: https://doaj.org/article/480798d68879446d8ecd3efe20d38d8a

المؤلفون: Emanuele Resta, Roberto Marsilio, Michele Ferlauto

المصدر: Fluids, Vol 6, Iss 12, p 441 (2021)

مصطلحات موضوعية: thrust vectoring, shock-vector control method, active flow control, supersonic nozzle, Thermodynamics, QC310.15-319, Descriptive and experimental mechanics, QC120-168.85

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2311-5521/6/12/441; https://doaj.org/toc/2311-5521

URL الوصول: https://doaj.org/article/f4717813692844f69133b1e635d1df90

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

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

مصطلحات موضوعية: optimal aerodynamic design, trapped vortex, vortex flow

وصف الملف: ELETTRONICO

Relation: ispartofbook:AIAA SCITECH 2024 Forum; AIAA SCITECH 2024 Forum; numberofpages:12; https://hdl.handle.net/11583/2984989; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85192140255; https://doi.org/10.2514/6.2024-0488

الاتاحة: https://hdl.handle.net/11583/2984989
https://doi.org/10.2514/6.2024-0488

المؤلفون: Emanuele Resta, Roberto Marsilio, Michele Ferlauto

مصطلحات موضوعية: aerospace propulsion, hot flows, computational fluid dynamics, rocket nozzles

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6a05e38e8c02f3bc8d0f76876974b72a
https://hdl.handle.net/11583/2975042

المؤلفون: Emanuele Resta, Michele Ferlauto, Roberto Marsilio

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

مصطلحات موضوعية: Air intake, shock wave, Artificial Intelligence

وصف الملف: ELETTRONICO

Relation: ispartofbook:International Conference on Computational Intelligence and Computing Applications-21 (ICCICA-21); International Conference on Computational Intelligence and Computing Applications-21 (ICCICA-21); volume:2424; firstpage:030005; numberofpages:6; serie:AIP CONFERENCE PROCEEDINGS; http://hdl.handle.net/11583/2958902; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85127530055

الاتاحة: http://hdl.handle.net/11583/2958902
https://doi.org/10.1063/5.0076817
https://aip.scitation.org/doi/abs/10.1063/5.0076817

المؤلفون: Emanuele Resta, Michele Ferlauto, Roberto Marsilio

المصدر: AIAA AVIATION 2022 Forum.

مصطلحات موضوعية: Aerospace Propulsion, Supersonic Nozzle, combustion, Thrust Vectoring, Supersonic Nozzle, Thrust Vectoring, Aerospace Propulsion, combustion

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60a0bfbe652e153bdb0a4b0738e9ae08
https://doi.org/10.2514/6.2022-3262