NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle TechnologyThis conference publication includes various abstracts and presentations given at the 13th Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology held at the George C. Marshall Space Flight Center April 25-27 1995. The purpose of the workshop was to discuss experimental and computational fluid dynamic activities in rocket propulsion and launch vehicles. The workshop was an open meeting for government, industry, and academia. A broad number of topics were discussed including computational fluid dynamic methodology, liquid and solid rocket propulsion, turbomachinery, combustion, heat transfer, and grid generation.
Document ID
19960029254
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Proceedings
Authors
Williams, R. W. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CP-3332-Vol-2
NAS 1:55:3332-Vol-2
Report Number: NASA-CP-3332-Vol-2
Report Number: NAS 1:55:3332-Vol-2
Meeting Information
Meeting: Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
Location: Huntsville, AL
Country: United States
Start Date: April 25, 1995
End Date: April 27, 1995
Accession Number
96N29750
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19960029275WorkA Coupled CFD/FEM Structural Analysis to Determine Deformed Shapes of the RSRM Inhibitors19960029256WorkSpatially Resolved Species Measurements in a GO2/GH2 Propellant Rocket19960029255WorkCombustion Zone Characterization of GO2/GH2 Rocket Using Laser-Induced Fluorescence of OH19960029270WorkA Structured Grid Based Solution-Adaptive Technique for Complex Separated Flows19960029278WorkCombustion Processes in Hybrid Rocket Engines19960029276WorkApplication of Two-Phase CFD to the Design and Analysis of a Subscale Motor Experiment to Evaluate Propellant Slag Production19960029263WorkApplication of Optimization Techniques to Design of Unconventional Rocket Nozzle Configurations19960029272WorkSurface and Volume Grid Generation in Parametric Form19960029264WorkTransonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept19960029260WorkA Parametric Study of a Plug Nozzle, Using the Liquid Propellant Program (LPP) Code19960029271WorkGENIE(++): A Multi-Block Structured Grid System19960029258WorkExperimental Investigation of the Effects of Acceleration on Heat Transfer in the Turbulent Boundary Layer19960029257WorkFluctuating Pressure Analysis of a 2-D SSME Nozzle Air Flow Test19960029265WorkAscent Aerodynamic Pressure Distributions on WB00119960029259WorkComputational and Experimental Efforts in Gravity Probe B Microthruster Analysis19960029267WorkTPS Sizing for Access-to-Space Vehicles19960029261WorkCFD Analysis of Modular Thrusters Performance19960029269WorkHybrid Grid Techniques for Propulsion Applications19960029268WorkComputational Issues Associated with Temporally Deforming Geometries Such as Thrust Vectoring Nozzles19960029277WorkNumerical Investigation of Slag Behavior for RSRM19960029262WorkPropellant Chemistry for CFD Applications19960029273WorkOverview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC19960029266WorkAssessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics19960029279WorkCFD Analysis of the 24-inch JIRAD Hybrid Rocket Motor19960029274WorkRSRM Chamber Pressure Oscillations: Transit Time Models and Unsteady CFD19960029255WorkCombustion Zone Characterization of GO2/GH2 Rocket Using Laser-Induced Fluorescence of OH19960029256WorkSpatially Resolved Species Measurements in a GO2/GH2 Propellant Rocket19960029257WorkFluctuating Pressure Analysis of a 2-D SSME Nozzle Air Flow Test19960029258WorkExperimental Investigation of the Effects of Acceleration on Heat Transfer in the Turbulent Boundary Layer19960029259WorkComputational and Experimental Efforts in Gravity Probe B Microthruster Analysis19960029260WorkA Parametric Study of a Plug Nozzle, Using the Liquid Propellant Program (LPP) Code19960029261WorkCFD Analysis of Modular Thrusters Performance19960029262WorkPropellant Chemistry for CFD Applications19960029263WorkApplication of Optimization Techniques to Design of Unconventional Rocket Nozzle Configurations19960029264WorkTransonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept19960029265WorkAscent Aerodynamic Pressure Distributions on WB00119960029266WorkAssessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics19960029267WorkTPS Sizing for Access-to-Space Vehicles19960029268WorkComputational Issues Associated with Temporally Deforming Geometries Such as Thrust Vectoring Nozzles19960029269WorkHybrid Grid Techniques for Propulsion Applications19960029270WorkA Structured Grid Based Solution-Adaptive Technique for Complex Separated Flows19960029271WorkGENIE(++): A Multi-Block Structured Grid System19960029272WorkSurface and Volume Grid Generation in Parametric Form19960029273WorkOverview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC19960029274WorkRSRM Chamber Pressure Oscillations: Transit Time Models and Unsteady CFD19960029275WorkA Coupled CFD/FEM Structural Analysis to Determine Deformed Shapes of the RSRM Inhibitors19960029276WorkApplication of Two-Phase CFD to the Design and Analysis of a Subscale Motor Experiment to Evaluate Propellant Slag Production19960029277WorkNumerical Investigation of Slag Behavior for RSRM19960029278WorkCombustion Processes in Hybrid Rocket Engines19960029279WorkCFD Analysis of the 24-inch JIRAD Hybrid Rocket Motor
No Preview Available