Add to ORKGThe Space Shuttle Orbiters Discovery and Endeavor have been digitally scanned to obtain outer mold line surfaces. Using these scans, the existing overset computational fluid dynamics (CFD) grid system will be modified by projecting the grid points to the scanned geometry. Simulations will be performed using the OVERFLOW solver and the results compared to previous OVERFLOW results on the theoretical geometry and the aerodynamic databook. The "bent airframe" term will be compared between the aerodynamic databook and the computations over a range of reentry conditions
An automated Computational Fluid Dynamics process for determining the aerodynamic Characteristics of...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
The Solid Rocket Motors (SRM) used by NASA to propel the Space Shuttle employ gimballing nozzles as ...
The Space Shuttle Orbiters Discovery and Endeavor have been digitally scanned to produce post-flight...
Numerical simulations using the thin-layer Navier-Stokes equations and chimera (overset) grid approa...
Algorithms and computer code developments were performed for the overset grid approach to solving co...
An enhanced grid system for the Space Shuttle Orbiter was built by integrating CAD definitions from ...
In support of the Columbia Accident Investigation, inviscid computations of the aerodynamic characte...
Topics are presented in viewgraph form and include the following: heavy lift launch vehicles, space ...
A viewgraph presentation on Computational Fluid Dynamic (CFD) Simulation of Space Shuttle Launch Veh...
The program to obtain intergrid communications - Pegasus - was enhanced to make better use of comput...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
Transonic aerodynamic analyses of a high aspect ratio wing-body model with curved planform are shown...
Computational fluid dynamics (CFD) analysis has provided verification of Space Shuttle flight perfor...
Modern Computational Fluid Dynamics (CFD) techniques were used to compute aerodynamic forces and mom...
An automated Computational Fluid Dynamics process for determining the aerodynamic Characteristics of...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
The Solid Rocket Motors (SRM) used by NASA to propel the Space Shuttle employ gimballing nozzles as ...
The Space Shuttle Orbiters Discovery and Endeavor have been digitally scanned to produce post-flight...
Numerical simulations using the thin-layer Navier-Stokes equations and chimera (overset) grid approa...
Algorithms and computer code developments were performed for the overset grid approach to solving co...
An enhanced grid system for the Space Shuttle Orbiter was built by integrating CAD definitions from ...
In support of the Columbia Accident Investigation, inviscid computations of the aerodynamic characte...
Topics are presented in viewgraph form and include the following: heavy lift launch vehicles, space ...
A viewgraph presentation on Computational Fluid Dynamic (CFD) Simulation of Space Shuttle Launch Veh...
The program to obtain intergrid communications - Pegasus - was enhanced to make better use of comput...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
Transonic aerodynamic analyses of a high aspect ratio wing-body model with curved planform are shown...
Computational fluid dynamics (CFD) analysis has provided verification of Space Shuttle flight perfor...
Modern Computational Fluid Dynamics (CFD) techniques were used to compute aerodynamic forces and mom...
An automated Computational Fluid Dynamics process for determining the aerodynamic Characteristics of...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
The Solid Rocket Motors (SRM) used by NASA to propel the Space Shuttle employ gimballing nozzles as ...