المؤلفون: Veivers, Harry, Bermingham, Michael, Dunn, Mitch, Veidt, Martin

المصدر: EA National Conference Publications; 2024, p129-141, 13p

مصطلحات موضوعية: LIGHTWEIGHT materials, ROCKET nozzles, PARTICLE swarm optimization, COMPUTER algorithms, STRESS concentration

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: Ahmed, Guelailia, Azzeddine, Khorsi, Ahmed, Slimane Sid, Hamza, Blala, Abdelkader, Slimane

المصدر: Trends in Sciences; Jul2023, Vol. 20 Issue 7, p1-9, 9p

مصطلحات موضوعية: TURBINE blades, ROCKET nozzles, SHEARING force, COOLING, COMBUSTION

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تسجيل الدخول للوصول الكامل.

المؤلفون: Jéger, Csaba, Veress, Á.

المصدر: Periodica Polytechnica Transportation Engineering. 47(2):131-135

مصطلحات موضوعية: CFD, Converging-diverging nozzle flow, Optimization, Rocket engine, Validation, Computational fluid dynamics, Geometry, Rocket engines, Rockets, Verification, Bell-shaped nozzle, Converging-diverging nozzles, Development process, Geometric optimization, Multiphysics systems, Nozzle pressure ratio, Parametric geometries, Rocket nozzles

وصف الملف: print

URL الوصول: https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-281269
https://doi.org/10.3311/PPtr.11490

المؤلفون: G. Anugrah, P. Raja, M. Deepu, R. Sadanandan

المصدر: Journal of Applied Fluid Mechanics, Vol 12, Iss 5, Pp 1719-1728 (2019)

مصطلحات موضوعية: Rocket nozzles, Thrust augmentation, HLLC scheme, Finite volume method., Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: http://jafmonline.net/JournalArchive/download?file_ID=49930&issue_ID=1002; https://doaj.org/toc/1735-3572

URL الوصول: https://doaj.org/article/86e2c2c46c3e4e6e86e0aac2cbde6ce4

المؤلفون: Stark, R.^Aff4, Génin, C.^Aff4

المساهمون: Ben-Dor, Gabi, editor^Aff1, Sadot, Oren, editor^Aff2, Igra, Ozer, editor^Aff3

المصدر: 30th International Symposium on Shock Waves 2 : ISSW30 - Volume 2. :1263-1267

المؤلفون: Srivastava, Nilabh, Tkacik, Peter T., Keanini, Russell G.

المصدر: Journal of Applied Physics; Sep2010, Vol. 108 Issue 4, p044911-91119, 19p, 3 Diagrams, 1 Chart, 13 Graphs

مصطلحات موضوعية: ROCKET nozzles, RIGID bodies, MATHEMATICAL models, ROCKET observations of the upper atmosphere, STOCHASTIC processes

المؤلفون: S. Shyji, M. Deepu, N. A. Kumar, T. Jayachandran

المصدر: Journal of Applied Fluid Mechanics, Vol 10, Iss 6, Pp 1605-1614 (2017)

مصطلحات موضوعية: Rocket nozzles, Thrust augmentation, Turbulent reacting flows, AUSM+-up scheme, Finite volume method., Mechanical engineering and machinery, TJ1-1570

وصف الملف: electronic resource

Relation: http://jafmonline.net/JournalArchive/download?file_ID=43816&issue_ID=245; https://doaj.org/toc/1735-3572

URL الوصول: https://doaj.org/article/ff6356d48b32474a974bc4b630d5695d

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