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PROJECTS RUNNING ON THE COLUMBIA SUPERCOMPUTER
Projects titles are listed in alphabetical order by principal investigator.
Aeronautics Mission Directorate
RANS & PANS for separated flow
Principal Investigator: Khaled S. Abdol-Hamid
Propulsion Airframe Aeroacoustics
Principal Investigator: Khaled S. Abdol-Hamid
Validation of RANS Flow Solver for the Slowed- Rotor Compound Helicopter Vehicle
Principal Investigator: Brian G. Allan
Separation Control Prediction for High-Lift
Principal Investigator: Brian G. Allan
Validstion of RANS Flow Solver for 3D Circ Control
Principal Investigator: Brian G. Allan
Unsteady Flow and Heat Transfer in Turbines
Principal Investigator: Ali A. Ameri
Pneumatic Control Effectors
Principal Investigator: Scott G. Anders
Advanced 'Fail Safe' Flow Control for the Next Generation Mixed Compression Supersonic Inlet
Principal Investigator: Bernhard Anderson
Roughness Induced Transistion in Hypesonic Boundary Layers
Principal Investigator: Ponnampalam Balakumar
Numerical Simulation of Transition in Supersonic Boundary Layers
Principal Investigator: Ponnampalam Balakumar
Quiet Supersonic Transport Computational Aeroelastic Investigation: Using CFL3D code
Principal Investigator: Robert E. Bartels
Deterministic and Statistical UQ for RANS Calculations
Principal Investigator: Timothy J. Barth
Supersonic Low-Boom/Low-Drag Computations
Principal Investigator: Steven X. S. Bauer
RAS and Hybrid RAS/LES of Hypersonic
Principal Investigator: Robert Baurle
Computational Materials for Hypersonics
Principal Investigator: Charles W. Bauschlicher Jr.
Hypersonics Systems Analysis
Principal Investigator: Glenn J. Bobskill
Computation of Jet Flow Interactions on Aeroshells
Principal Investigator: Iain D. Boyd
Hybrid Continuum-Particle Simulations of Hypersonic Entry Flows
Principal Investigator: Iain D. Boyd
Turbine Heat Transfer
Principal Investigator: Robert J. Boyle
CFD Study of the Sonic Boom Characteristics of the NASA F-16XL
Principal Investigator: Trong T. Bui
CFD Study of the Sonic Boom Characteristics of the Northrop Grumman Oblique Flying Wing
Principal Investigator: Trong T. Bui
Study of the NASA F-15B Engine Nozzle Area Ratio Effects on the Supersonic Aircraft Aft Shock
Principal Investigator: Trong T. Bui
3D Hydrocarbon Scramjet Combustor Analysis
Principal Investigator: Michael Bynum
Low-Sweep Transonic Wing Design
Principal Investigator: Richard L. Campbell
High-Resolution RANS/DES Code Development and Applications for Aeromechanics Simulations
Principal Investigator: Neal M. Chaderjian
Hypersonics Unsteady Viscous Flow over Large Roughness Elements
Principal Investigator: Dr. Chau-Lyan Chang
Compressor Stall Modeling
Principal Investigator: Dr. Rodrick V. Chima
Transition Physics and Modeling
Principal Investigator: Dr. Meelan M. Choudhari
Computational Materials Modeling of Aircraft Aging and Durability
Principal Investigator: Thomas Clancy
High-Fidelity Engine Simulation
Principal Investigator: Russell W. Claus
High Fidelity Engine Simulation
Principal Investigator: Russell W. Claus
EDL and Design Optimization at Supersonic Conditions
Principal Investigator: Susan E. Cliff
Unstructured Euler-Based Analysis and Design for Fixed Wing Aircraft
Principal Investigator: Susan E. Cliff
Computational Methods for Low-Noise Supersonic Nozzle Development
Principal Investigator: James R. DeBonis
Computational Investigation of an Advanced Dual Throat, Fluidic Thrust Vectoring Nozzle
Principal Investigator: Karen A. Deere
Computational Investigation of a Circulation Control etc..
Principal Investigator: Karen A. Deere
Rotorcraft Computations - Ames
Principal Investigator: Daniel Dugan
Supersonic Cruise Efficiency/Airframe & EDL Technologies
Principal Investigator: Donald A. Durston
Development of Hybrid Large-Eddy/Reynolds AveragesNavier-Stokes Methods for High-Speed Internal Flow
Principal Investigator: Jack R. Edwards
Multi-Scale Modeling of Mult-Functional Composites
Principal Investigator: Sarah-Jane Frankland
Multifunctional Nanostructures
Principal Investigator: Sarah-Jane Frankland
Investigations of Detached Eddy Simulation and Dynamic Grids for S&C Problems Using TetrUSS
Principal Investigator: Dr. Neal T. Frink
3D RANS Calculations of the DCR Experiment
Principal Investigator: Richard Gaffney
Computational Materials
Principal Investigator: Thomas Gates
Modeling and Simulation in Support of Test and Evaluation
Principal Investigator: Nicholas J. Georgiadis
Hypersonic Simulations on Unstructured Grid
Principal Investigator: Peter A. Gnoffo
Large Eddy Simulation for Highly Loaded Turbomachinery
Principal Investigator: Dr. Chunill Hah
Large Eddy Simulation for Compressor Flow Control
Principal Investigator: Dr. Chunill Hah
Unsteady Circulation Control For High-Performance Low-Noise Aircraft
Principal Investigator: Andreas Haselbacher
Integrated Inlet/Fan Simulation
Principal Investigator: Michael D. Hathaway
Numerical Simulation of Multistage Turbomachinery Flows
Principal Investigator: Michael D. Hathaway
Multistage CFD of Turbomachinery
Principal Investigator: James D. Heidmann
Numerical Simulation of Advanced Turbine Cooling Concepts
Principal Investigator: James D. Heidmann
Detailed Modeling of Combustion Noise Using a Combined Large-Eddy Simulation/Computational
Principal Investigator: Lennart Hultgren
Foreign National Access-17 High-Fidelity NumericalSimulations of Jet and Airframe Acoustics
Principal Investigator: Lennart Hultgren
Engine Noise CFO
Principal Investigator: Philip Jorgenson
Development of Next Generation Flow Codes for Supersonic EDL Systems
Principal Investigator: Upender K. Kaul
CFD Analyis of Circ Control Effectiveness
Principal Investigator: Edwin Koshimoto
Automation in Multi Displinary Analysis and DesignOptimization for a Supersonic Variable Sweep Wing
Principal Investigator: May-Fun Liou
Design Optimization of Turbomachinery Using Genetic Algorithms
Principal Investigator: Meng-Sing Liou
Foreign National Access-808
Principal Investigator: Meng-Sing Liou
Validation of the National Combustion Code (NCC)
Principal Investigator: Nan-Suey Liu
Foreign National Access-15
Principal Investigator: Nan-Suey Liu
National Combustion Code (NCC) Application and Design
Principal Investigator: Nan-Suey Liu
Kinetic Eddy Simulation of Multi-phase Turbulent Combustion
Principal Investigator: Nan-Suey Liu
Foriegn National Access-814
Principal Investigator: Nan-Suey Liu
Sonic Boom Propagation through Turbulence
Principal Investigator: Lance Locey
Landing Gear Noise Modeling
Principal Investigator: David P. Lockard
Turbulent Flows Simulation of Helicopter Fuselage Flow Fields
Principal Investigator: Lyle N. Long
Rotorcraft Propulsion
Principal Investigator: Isaac Lopez
X-51 Aerodynamics
Principal Investigator: Todd E. Magee
Boundary Layer Transition and Laminar Flow Control
Principal Investigator: Dr. Mujeeb R. Malik
Foreign National Access-805
Principal Investigator: Nagi N. Mansour
Molecular Dynamics Simulations of Gas Surface Interactions
Principal Investigator: Nagi N. Mansour
Hypersonics Project: Entry, Descent, and Landing (EDL) Simulations
Principal Investigator: Nagi N. Mansour
Fundamental Aero-Hypersonics
Principal Investigator: Nagi N. Mansour
NRA: DNS of Turbulent Hypersonic Wall-Bounded Flows including Real Gas Effects and Surface Inter
Principal Investigator: Pino Martin
Numerical Investigation of Transition in Supersonic Flows
Principal Investigator: Christian Mayer
ATK Robust Scramjet
Principal Investigator: Keith McDaniel
LES of a Combustion Powered Actuator (COMPACT)
Principal Investigator: Dr. Suresh Menon
Circulation Control Aerodynamics
Principal Investigator: William E. Milholen
Computational Support for Drag Prediction Workshop
Principal Investigator: Joseph H. Morrison
Average-Passage Simulation of Turbomachinery
Principal Investigator: Richard A. Mulac
ARMD/Hypersonics (HSA) project: Soarex
Principal Investigator: Marcus Murbach
High-Fidelity Simulations of High-Mass Mars-entry Capsules
Principal Investigator: Scott M. Murman
NASA Advanced Satellite Aviation-Weather Products (ASAP) in Flight Icing
Principal Investigator: Louis Nguyen
Combustion Code Development
Principal Investigator: Andrew T. Norris
Hypersonic Propulsion Simulation
Principal Investigator: Andrew T. Norris
Control Effectors for Supersonic Tailless Aircraft
Principal Investigator: Lewis R. Owens
Supersonics Multifidelity Low Boom Design
Principal Investigator: Lori Ozoroski
Computational Support for LaNCETS Flight Test
Principal Investigator: Lori Ozoroski
HRLS CFD Analysis
Principal Investigator: Jenn L. Pao
Ejector-Based Unsteady Pressure-Gain Combustors
Principal Investigator: Daniel Paxson
Foreign National Access-IX High-Fidelity NumericalSimulations of Jet and Airframe Acoustics
Principal Investigator: Kimlan T. Pham
University Research Engineering Technology Institute (URET)
Principal Investigator: Kimlan T. Pham
High-Fidelity Numerical in Jet Aeroacoustics with Application to Chevron Nozzles and High-Fidelity
Principal Investigator: Kimlan T. Pham
Advanced Methods for Large-Scale Unstructured Grid Generation
Principal Investigator: Dr. Shahyar Pirzadeh
Parametric Studies of Aircraft Wake Decay and Transport
Principal Investigator: Fred H. Proctor
Generation of CFD Data Sets for Airborne Sensor Evaluation of Airborne Hazards
Principal Investigator: Fred H. Proctor
Simulation of Turbine Blade Heat Transfer
Principal Investigator: Dr. David L. Rigby
NASA Ames Computational Research for FA-SFW
Principal Investigator: Dr. Michael M. Rogers
International Visitor Access-816
Principal Investigator: Dr. Michael M. Rogers
Circulation Control for High Lift
Principal Investigator: Christopher L. Rumsey
Computational Aerosciences of Advanced Aircraft
Principal Investigator: Michael J. Schuh
Flowpath Integration for TBCC and RBCC Propulsion Systems
Principal Investigator: Matt Sexton
Direct and Large-Eddy Simulation of an Circulation
Principal Investigator: Karim R. Shariff
Quiet Supersonic Transport Computational Aero- elastic Investigation: Using Reduced-order Model
Principal Investigator: Walter A. Silva
Computational Aero Elasticity for Supersonic Configurations
Principal Investigator: Walter A. Silva
Transonic Aeroelastic Analysis of the SemiSpan SuperSonic Transport Model
Principal Investigator: Walter A. Silva
Detached-Eddy Simulation in the Boeing 777 Nose-Gear Cavity
Principal Investigator: Dr. Philippe R. Spalart
Hypersonic Flow Simulations
Principal Investigator: R. Charles Swanson
Simulations of Pulse Detonation Engine-Turbine Interactions
Principal Investigator: Venkat Tangirala
B757 CFD Analysis
Principal Investigator: Joseph Totah
Hypersonic Air Breathing Vehicles
Principal Investigator: Erik D. Tyler
Engine Turbine Noise Simulation Study-2
Principal Investigator: Dale Van Zante
Engine Turbine Noise Simulation Study-1
Principal Investigator: Dale Van Zante
Foreign National Access-802
Principal Investigator: Meng Wang
LES of airframe noise control using plasma actuators
Principal Investigator: Meng Wang
Duct Acoustics Modeling
Principal Investigator: Willie R. Watson
Rotorcraft Computations-Langley
Principal Investigator: Michael E. Watts
Foreign National Access-VIII
Principal Investigator: Michael E. Watts
Post-Combustor Gaseous and Particulate Matter Emissions
Principal Investigator: Thomas C. Wey
Coupled RANS/LES for Cavity Acoustic Prediction
Principal Investigator: Stephen Woodruff
CFD Analysis of FADS Performance During Launch and Re-entry of Space Vehicles
Principal Investigator: Stephen Woodruff
Modeling in Aerodynamics, Aerothermodynamics and Plasma Physics
Principal Investigator: Seokkwan Yoon
Hypersonics-Propulsion Modeling
Principal Investigator: Shaye Yungster
Speed up MP4 Calculations Through Multiprocessor NWCHEM
Principal Investigator: Michael J. Zehe
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Last Updated: May 8, 2008