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A Mesh Generation Template for Turbomachinery Blade Passages
An Analytical Investigation of the Effects of Stator Airfoil Clocking on Turbine Performance
A Parametric Study of a Plug Nozzle Using the Liquid Propellant Program (LPP) Code
Application of Optimization Techniques to Design of Unconventional Rocket Nozzle Configurations
Ascent Aerodynamic Pressure Distributions on WB001
Assessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics
CFD Analysis in the Design of a Water-Jet-Drive System
CFD Analysis of Modular Thrusters Performance
CFD Analysis of the 24-Inch Jirad Hybrid Rocket Motor
CFD Analysis of the ATD HPFTP Inlet Guide Vanes
CFD Flow Analysis and Code Validation for the MSFC Eight-Percent ASRM Cold Flow Model Part II
Combustion Processes in Hybrid Rocket Engines
Combustion Zone Characterization of GO~2/GH~2 Rocket Using Laser-Induced Fluorescence of OH
Combustor Modeling Under Gox-Rich Conditions
Computational Analysis of Volutes
Computational and Experimental Efforts in Gravity Probe B Microthruster Analysis
Fluctuating Pressure Analysis of a 2-D SSME Nozzle Air Flow Test
Gas/Gas Injector Technology Program
Genie++ - A Multi-Block Structured Grid System
Hybrid Grid Techniques for Propulsion Applications
Influence of Tip Clearance and Reynolds Number on the Flow in the ADP Inducer
Numerical Investigation of Slag Behavior for RSRM
Numerical Modeling of Spray Combustion with an Unstructured-Grid Method
Numerical Simulation of Diffuser Flow
Optimization Methodology for Unconventional Rocket Nozzle Design
Overview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC
Overview of MSFC CFD Activities
Oxygen-Rich Combustion Experiments in a LOX/GH~2 Uni-Element Rocket
Process Demonstration and React Code Validation for Shrouded Inducer Operation at and Off Design
Progress Towards an Efficient and General CFD Tool for Propulsion Design/Analysis
Propellant Chemistry for CFD Applications
Reusable Launch Vehicle (RLV) Propulsion Technology
Rocketdyne's Turbomachinery Design Process Improvements for RRTT and Future Programs
RSRM Chamber Pressure Oscillations: Transit Time Models and Unsteady CFD
Spatially Resolved Species Measurements in a GO~2/GH~2 Propellant Rocket
Surface and Volume Grid Generation in Parametric Form
TPS Sizing for Access-to-Space Vehicles
Transonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept
Turbulence Modeling and Computation of Turbine Aerodynamics and Heat Transfer
Zero Side Force Volute Development