A model of the wind flow conditions around Kennedy Space Center (KSC) Vehicle Assembly Building (VAB) is presented. An incompressible Navier-Stokes flow solver was used to compute the flow field around fixed Launch Complex 39 (LC-39) buildings and structures. The 3-D flow field, including velocity magnitude and velocity vectors, was established to simulate the localized wind speeds and directions at specified locations in and around LC-39 buildings and structures. The results of this study not only help explain the physical phenomena of the flow patterns around LC-39 buildings but also are useful to the Shuttle personnel. Current Operations and Maintenance Requirements and Specifications (OMRS) for vehicle transfer operations are based on empirically derived historical data, and no detailed mathematical analysis of wind conditions around LC-39 structures has ever been accomplished.
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ASME 2004 Heat Transfer/Fluids Engineering Summer Conference
July 11–15, 2004
Charlotte, North Carolina, USA
Conference Sponsors:
- Heat Transfer Division and Fluids Engineering Division
ISBN:
0-7918-4691-1
PROCEEDINGS PAPER
Wind Flow Simulation Around NASA KSC Vehicle Assembly Building Available to Purchase
B. T. Vu,
B. T. Vu
NASA Kennedy Space Center, Kennedy Space Center, FL
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M. J. Verdier
M. J. Verdier
NASA Kennedy Space Center, Kennedy Space Center, FL
Search for other works by this author on:
B. T. Vu
NASA Kennedy Space Center, Kennedy Space Center, FL
M. J. Verdier
NASA Kennedy Space Center, Kennedy Space Center, FL
Paper No:
HT-FED2004-56855, pp. 1315-1318; 4 pages
Published Online:
February 24, 2009
Citation
Vu, BT, & Verdier, MJ. "Wind Flow Simulation Around NASA KSC Vehicle Assembly Building." Proceedings of the ASME 2004 Heat Transfer/Fluids Engineering Summer Conference. Volume 2, Parts A and B. Charlotte, North Carolina, USA. July 11–15, 2004. pp. 1315-1318. ASME. https://doi.org/10.1115/HT-FED2004-56855
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