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1 Ergebnisse
1
A Simplified Thermal Analysis Model for Regeneratively Cool..:
Matteo Fagherazzi
;
Marco Santi
;
Francesco Barato
.
https://www.mdpi.com/2226-4310/10/5/403. , 2023
Link:
https://doi.org/10.3390/aerospace10050403
RT Journal T1
A Simplified Thermal Analysis Model for Regeneratively Cooled Rocket Engine Thrust Chambers and Its Calibration with Experimental Data
UL https://suche.suub.uni-bremen.de/peid=base-ftdoajarticles:oai:doaj.org_article:5b4a44f1889b4730bff2b0b88579edfd&Exemplar=1&LAN=DE A1 Matteo Fagherazzi A1 Marco Santi A1 Francesco Barato A1 Marco Pizzarelli PB MDPI AG YR 2023 K1 rocket engine thrust chamber K1 regenerative cooling K1 cooling channel K1 hydrogen peroxide K1 additive manufacturing K1 heat transfer modeling K1 Motor vehicles. Aeronautics. Astronautics K1 TL1-4050 JF https://www.mdpi.com/2226-4310/10/5/403 LK http://dx.doi.org/https://doi.org/10.3390/aerospace10050403 DO https://doi.org/10.3390/aerospace10050403 SF ELIB - SuUB Bremen
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