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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