Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Justin Oliveira"'
Publikováno v:
Sports Engineering. 25
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::20326cadac96a4a9029f30991625938f
https://doi.org/10.1007/s12283-022-00375-4
https://doi.org/10.1007/s12283-022-00375-4
Autor:
Félix Croteau, Brian Parillo, Thomas Romeas, Justin Oliveira, Alain Delorme, Nicolas Berryman, David Paradelo, Lily Dong, Evelyne Dubé, François Bieuzen, François Billaut
Publikováno v:
Journal of strength and conditioning research. 35(Suppl 2)
Dong, L, Paradelo, D, Delorme, A, Oliveira, J, Parillo, B, Croteau, F, Romeas, T, Dube, E, Bieuzen, F, Billaut, F, and Berryman, N. Sport-specific agility and change of direction in water polo: The reliability and validity of two newly developed test
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5190568e10da86165037ddb1434fc013
https://pubmed.ncbi.nlm.nih.gov/34846332
https://pubmed.ncbi.nlm.nih.gov/34846332
Effect of Isogrid-Type Obstructions on Thermal Stratification in Upper-Stage Rocket Propellant Tanks
Publikováno v:
Journal of Spacecraft and Rockets. 51:1587-1602
Analytical models for propellant thermal stratification are typically based on smooth wall flow correlations. However, many propellant tank walls have a mass-saving isogrid, which alters the boundary layer. This work investigates the boundary-layer b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f62b89be94f2bcceddb474355666e22c
https://doi.org/10.2514/1.a32699
https://doi.org/10.2514/1.a32699
Publikováno v:
Journal of Spacecraft and Rockets. 46:459-465
Modeling the thermal behavior of cryogenic propellants within the upper stages of a launch vehicle is necessary for successful mission planning. During orbital transfer, the upper stage may coast for several hours, during which the propellants are he
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3244b19fd956493d1981f714ca245f9c
https://doi.org/10.2514/1.39760
https://doi.org/10.2514/1.39760
Publikováno v:
20th AIAA Computational Fluid Dynamics Conference.
This paper describes the Computation Fluid Dynamics (CFD) model developed to simulate the supersonic rocket exhaust in an entrained flow cylinder. The model can be used to study the plume-induced environment due to static firing test of the Taurus II
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf6dcb4d10cc0ae406c179320a459eca
https://doi.org/10.2514/6.2011-3210
https://doi.org/10.2514/6.2011-3210
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Modeling the thermal stratification of cryogenic propellants within the upper stage of a launch vehicle is necessary for mission planning and successful execution. During orbital transfer the upper stage may coast for several hours during which time
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8f9517cd5928c5bee57ea89989fc6626
https://doi.org/10.2514/6.2007-5495
https://doi.org/10.2514/6.2007-5495
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Payloads requiring insertion into high altitude orbits are delivered using the upper stages of chemical rockets (ex., Delta and Atlas classes) normally employing cryogenic propellants. During the transfer period between orbits, the upper stage may co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70a4fce2f6392e6deb3f79fb887f1683
https://doi.org/10.2514/6.2007-5497
https://doi.org/10.2514/6.2007-5497
Publikováno v:
37th AIAA Fluid Dynamics Conference and Exhibit.
Payloads requiring insertion into high altitude orbits are delivered using the upper stages of chemical rockets (ex., Delta and Atlas classes) normally employing cryogenic propellants. During the transfer period between orbits, the upper stage may co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86c8a5186235d3f7d6d978fdaf2583d4
https://doi.org/10.2514/6.2007-4479
https://doi.org/10.2514/6.2007-4479
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Payloads requiring insertion into high altitude orbits are delivered using the upper stages of chemical rockets (ex., Delta and Atlas classes) normally employing cryogenic propellants. During the transfer period between orbits, the upper stage may co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c97ceb7aedfb7180704b099a09a6f0ce
https://doi.org/10.2514/6.2006-5059
https://doi.org/10.2514/6.2006-5059
Publikováno v:
Harvard Business School Cases. Jan 01, 2019, p1. 16p.