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Supersonics Project
The goal of the Supersonics project is to conduct long-term,
cutting-edge research in the core competencies of the supersonic regime,
thereby producing knowledge, data, capabilities, technologies, and
design tools at the foundational, discipline, multidiscipline and
systems levels that will address the technical challenges for two
supersonic vehicle classes: practical supersonic cruise vehicles and
High Mass Mars Entry Systems.
The project is organized along the following major technical challenges
that have been identified for the two vehicle classes: efficiency
(supersonic cruise, light weight and durability at high temperature);
environmental challenges (airport noise, sonic boom, high altitude
emissions); performance challenges (aero-propulso-servo-elastic analysis
and design); entry descent and landing challenges (supersonic
deceleration); and multidisciplinary design, analysis and optimization
challenges.
The following are ROA-2007 NRA awards for the Supersonics Project, with the most recent listed first.
+ ROA-2007 Supersonics Project NRA Awards (click to open and close panel)

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Bobbitt |
The Measurement of Free-Stream Mach Number, Pressure, Temperature, Density and Angle-of-Attack at Supersonic Speeds Using a Conical and Wedge Probes |
Eagle Aeronautics Inc |
VA |
06/18/2008 |
$130,000 |
| Madenci |
Peridynamic Modelling of Three-Dimensional Damage Growth in Metallic and Composite Aerospace Structures |
University of Arizona |
AZ |
05/07/2008 |
$317,000 |
| Loth |
Development of a Large-Scale Low-Boom Supersonic Inlet for Investigating Micro-Array Flow Control |
University of Illinois at Urbana-Champaign |
IL |
03/26/2008 |
$459,504 |
| Mortlock |
Subtopic A.4.7.4 System Level Experimental Validations |
The Boeing Company |
CA |
03/26/2008 |
$784,235 |
| Welge |
Supersonic Concept Development and System Studies |
The Boeing Company |
CA |
03/26/2008 |
$1,271,085 |
| Marshall |
3D Fiber Architectures for Thin-walled Ceramic Composite Turbine Airfoil Components |
Teledyne Scientific Company |
CA |
02/01/2008 |
$201,000 |
| Sharp |
3-D Braided Ceramic Fiber Vane Preforms |
3TEX |
NC |
01/17/2008 |
$190,314 |
| McLaughlin |
Multipoint Flow and Acoustic Diagnostic Experiments for Source Modeling in Supersonic Jets |
Pennsylvania State University |
PA |
01/10/2008 |
$211,902 |
| Hamed |
Computational Bleed Model for Supersonic Inlets |
University of Cincinnati |
OH |
01/10/2008 |
$195,593 |
| Jimerson |
High Fidelity Supersonic Exhaust System Design and Validation Model |
Rolls-Royce North American Technologies Inc. |
IN |
12/21/2007 |
$197,129 |
| Clark |
Laminar Flow Technology for Supersonic Transport Aircraft |
The Boeing Company |
CA |
12/21/2007 |
$245,358 |
| Plotkin |
Low Boom Supersonic Vehicle Shaping Tools |
Wyle Laboratories |
VA |
12/21/2007 |
$180,246 |
| Gilat |
Temperature and Strain Rate effects on the Deformation and Failure of Advanced High-Temperature Polymer Resins and 3-D Fiber Preform Reinforced Polymer Matrix Composites (PMCs) |
Ohio State University |
OH |
11/27/2007 |
$336,000 |
| Ned |
Fully Integrated Miniature, High Frequency Flow Probe Utilizing Advanced MEMS, Leadless SOI Technology |
Kulite Semiconductor Products, Inc. |
NJ |
11/27/2007 |
$292,150 |
| Vaidyanathan |
Development and Characterization of High-Temperature Shape Memory Alloys with in situ Neutron Diffraction Measurements at Temperature and Stress |
University of Central Florida |
FL |
11/20/2007 |
$194,000 |
| Annen |
High Speed Temperature Analysis Software and Support for Temporally-Resolved Laser Raman Temperature Measurements in a Supersonic Jet |
Aerodyne Ressearch, Inc |
MA |
11/14/2007 |
$196,415 |
| Mills |
A Microstructure-Based Approach to Develop New High Temperature Shape Memory Alloys |
Ohio State University |
OH |
11/13/2007 |
$256,572 |
| Corke |
Plasma Bumps for Cross-Flow Turbulent Transition Prediction and Control |
University of Notre Dame |
IN |
11/13/2007 |
$175,000 |
| Weir |
Design and Fabrication of Modifications to a Mach 2.5 Supersonic Mixed-Compression Inlet Model for Validation of Micro-Ramp Flow Control Devices in the NASA GRC 10x10 SWT |
TechLand Research, Inc. |
OH |
10/31/2007 |
$305,077 |

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The following are ROA-2006 NRA awards for the Supersonics Project, with the most recent listed first.
+ ROA-2006 Supersonics Project Awards (click to open and close panel)

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Baldelli |
CFD-Based Aeroservoelastic Methodology for Supersonic Aircraft Flutter Suppression Gust Loads Alleviation, and Ride Quality Augmentation |
Zona Technology, Inc |
AZ |
09/27/2007 |
$199,721 |
| Baker |
Simultaneous Flutter Suppression, Gust Load Alleviation, and Ride Quality Augmentation for Supersonic Aircraft at Transonic Conditions |
M4 Engineering Inc |
CA |
09/25/2007 |
$250,000 |
| Burdisso |
Development of a Model for Predicting the Transmission of Sonic Booms into Buildings |
Virginia Polytechnic Institute & State University |
VA |
08/30/2007 |
$185,469 |
| Sizov |
Modeling of Rattle and Other Contact Induced Noise |
Wyle Laboratories, Inc. |
VA |
08/21/2007 |
$197,920 |
| Sizov |
Transmission of sonic boom into building structures |
Wyle Laboratories, Inc. |
VA |
08/21/2007 |
$140,029 |
| Page |
Atmospheric Sonic Boom Prediction Model |
Wyle Laboratories, Inc. |
VA |
08/16/2007 |
$219,687 |
| Sparrow |
Low-Boom Sonic Boom Coupled Diffraction Around And Transmission Through Individual And Aggregated Building Structures |
Pennsylvania State University |
PA |
07/10/2007 |
$99,000 |
| Kroo |
Multifidelity Analysis and Design Methods for Supersonic Aircraft |
Stanford University |
CA |
02/27/2007 |
$302,000 |
| Ameri |
Development of a High Fidelity Multi-Disciplinary Conjugate Heat Transfer Module for Incorporation into a NASA Computer Code. |
Ohio State University |
OH |
02/27/2007 |
$220,000 |
| Yamaleev |
Adjoint-based Methodology for Time-dependent Optimal Control (AMTOC) |
National Institute of Aerospace |
VA |
02/12/2007 |
$283000 |
| Karman |
A Generalized Framework for Constrained Design Optimization of General Supersonic Configurations Using Adjoint Based Sensitivity Derivatives |
The University Of Tennessee |
TN |
01/31/2007 |
$205,000 |
| Collier |
A Multiscale, Validated, Physics-Based Progressive Failure Modeling Tool For Advanced Composite Structures |
Collier Research And Development Corporation |
VA |
01/31/2007 |
$236,000 |
| Samimy |
Supersonic Jet Noise Suppression Using Plasma Actuators: Coupled Experiments, Les And Adjoint-Based Optimization |
The Ohio State University Research Foundation |
OH |
01/29/2007 |
$281,000 |
| Fasel |
Transition in High-Speed Boundary Layers: Numerical Investigations using DNS and LES |
University Of Arizona |
AZ |
01/27/2007 |
$199,000 |
| Lele |
Prediction And Modeling Of Supersonic Jet Noise Using Large-Eddy Simulation |
Leland Stanford Junior University |
CA |
01/27/2007 |
$326,000 |
| Tewari |
Strain-Tolerant Self-Sensing Environmental Barrier Coatings For SiC/SiC Ceramic Matrix Composites And Si3N4 Ceramics |
Cleveland State University |
OH |
01/27/2007 |
$205,000 |
| Fotache |
Validated Computational Tools For Low Emissions Injector Design Using Superheated/Supercritical Fuels |
United Technologies Research Center |
CT |
01/26/2007 |
$294,000 |
| Lucht |
Coherent Anti-Stokes Raman Scattering (CARS) For Quantitative Temperature And Concentration Measurements In A High-Pressure Gas Turbine Combustion Test Rig |
Purdue University |
ID |
01/25/2007 |
$273,000 |
| Loos |
Modeling The Vacuum Assisted Resin Transfer Molding Process For Fabrication Of Fiber/Metal Hybrid Laminates |
Michigan State University |
MI |
01/25/2007 |
$116,000 |
| Pitsch |
Emissions Prediction And Modeling Of Supersonic Vehicle Combustion Systems |
Leland Stanford Junior University |
CA |
01/20/2007 |
$343,000 |
| Loth |
SBLI Flow Control With Micro-VG'S Using LES |
University Of Illinois |
IL |
01/20/2007 |
$84,000 |
| Kojima |
Time-Resolved Laser Raman Spectroscopy For Scalar Measurements Of Swirl-Stabilized Liquid-Fueled Combustion At Elevated Pressures And Temperatures: Toward Combustion Code Validation |
Ohio Aerospace Institute |
OH |
01/20/2007 |
$141,000 |
| Santavicca |
Active Combustion Control For Supersonic Low Emission Combustors |
The Pennsylvania State University |
PA |
01/20/2007 |
$320,000 |
| Morris |
A Comprehensive Model For The Prediction Of Supersonic Jet Noise |
The Pennsylvania State University |
PA |
01/20/2007 |
$232,000 |
| Bogard |
Experimental Measurements And Computational Predictions Of Conjugate Heat Transfer In A Stationary Cooled Turbine Vane |
University Of Texas At Austin |
TX |
01/20/2007 |
$264,000 |
| Papamoschou |
Supersonic Jet Noise Reduction Via Reshaping Of The Exhaust Plume |
University Of California (Irvine Campus) |
CA |
01/16/2007 |
$213,000 |
| Seitzman |
Detection And Control Of Instabilities And Blowoff For Low Emissions Combustors |
Georgia Tech Research Corp |
GA |
01/16/2007 |
$256,000 |
| Roy |
Life Prediction Of Composite Materials Subjected To Long-Term Mechanical/Environmental Loading Conditions |
The University Of Alabama |
AL |
01/05/2007 |
$141,000 |
| Darmofal |
Development And Application Of A Higher-Order, Adaptive Method For Aerodynamic And Sonic-Boom Design Of Supersonic Aircraft |
Massachusetts Institute Of Technology |
MA |
12/22/2006 |
$296,000 |
| Tippur |
Investigation Of Strain-Rate Effects On Crack Growth In Graphite-Epoxy Composites With Stiffeners |
Auburn University |
AL |
12/21/2006 |
$174,000 |

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+ Subsonic Fixed Wing Project
+ Subsonic Rotary Wing Project
+ Supersonics Project
+ Hypersonics Project
+ Entry, Descent and Landing (EDL) (Joint Hypersonics/Supersonics)
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