A model of the wind flow conditions around Kennedy Space Center (KSC) Vehicle Assembly Building (VA B) 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 ...
This report describes the results of wind tunnel experiments and numerical simulations about the flo...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel ...
Includes bibliographical references.September 1982.CER82-83JAP-JEC13.For Martin Marietta Corporation...
ABSTRACT Since atmospheric winds play the most critical natural enviroment (NE) role as input into t...
In an attempt to explain the high loss of panels from the south face of the Vehicle Assembly Buildin...
The authors compare the results of computer simulated flow fields around a complex building (B170) a...
The authors compare the results of a computer simulated flow field around building 170 (B170) at Law...
Turbulence in the wake generated by wind flow over buildings or obstacles may produce complex flow p...
This paper discusses the Space Shuttle Lift-Off CFD model developed for potential Lift-Off Debris tr...
Physical and mathematical models for studying erected launch vehicle response to ground wind
ABSTRACT This paper presents a wind tunnel study of the flow patterns in the main Brazilian Space Po...
The aerodynamics around space launch vehicles determine the external forces that these vehicles expe...
Wind loads are of important, particularly in the design of large structures. The wind velocity that ...
The use of computational fluid dynamics has risen in the past decade. With major advances in high pe...
This report describes the results of wind tunnel experiments and numerical simulations about the flo...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel ...
Includes bibliographical references.September 1982.CER82-83JAP-JEC13.For Martin Marietta Corporation...
ABSTRACT Since atmospheric winds play the most critical natural enviroment (NE) role as input into t...
In an attempt to explain the high loss of panels from the south face of the Vehicle Assembly Buildin...
The authors compare the results of computer simulated flow fields around a complex building (B170) a...
The authors compare the results of a computer simulated flow field around building 170 (B170) at Law...
Turbulence in the wake generated by wind flow over buildings or obstacles may produce complex flow p...
This paper discusses the Space Shuttle Lift-Off CFD model developed for potential Lift-Off Debris tr...
Physical and mathematical models for studying erected launch vehicle response to ground wind
ABSTRACT This paper presents a wind tunnel study of the flow patterns in the main Brazilian Space Po...
The aerodynamics around space launch vehicles determine the external forces that these vehicles expe...
Wind loads are of important, particularly in the design of large structures. The wind velocity that ...
The use of computational fluid dynamics has risen in the past decade. With major advances in high pe...
This report describes the results of wind tunnel experiments and numerical simulations about the flo...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel ...