Analysis of Convective Heat Transfer in the Orbiter Middeck for the Shuttle Rescue Mission 2009-01-2550
The paper presents the results of a CFD study for predictions of ventilation characteristics and convective heat transfer within the Shuttle Orbiter middeck cabin in the presence of seven suited crewmember simulation and Individual Cooling Units (ICU). For two ICU arrangements considered, the thermal environmental conditions directly affecting the ICU performance have been defined for landing operation. These data would allow for validation of the ICU arrangement optimization.
Citation: Son, C., Dunaway, B., Smirnov, E., Ivanov, N. et al., "Analysis of Convective Heat Transfer in the Orbiter Middeck for the Shuttle Rescue Mission," SAE Int. J. Aerosp. 4(1):525-530, 2011, https://doi.org/10.4271/2009-01-2550. Download Citation
Author(s):
Chang H. Son, Brian R. Dunaway, Evgueni M. Smirnov, Nikolay G. Ivanov, Denis S. Telnov
Affiliated:
The Boeing Company, New Technologies and Services, Russia
Pages: 6
Event:
International Conference On Environmental Systems
ISSN:
1946-3855
e-ISSN:
1946-3901
Also in:
SAE International Journal of Aerospace-V120-1, SAE International Journal of Aerospace-V120-1EJ
Related Topics:
Heat transfer
Computational fluid dynamics
Optimization
Simulation and modeling
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