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Hypersonics Project
The Hypersonics Project is motivated by the fact that all access to
Earth or planetary orbit, and all entry from orbit into Earth's
atmosphere or any planet with an atmosphere, requires flight through the
hypersonic regime. The goal of the project is to conduct long-term,
cutting-edge research in the core competencies of the hypersonic regime,
thereby producing knowledge, data, capabilities, and design tools at the
foundational, discipline, multidiscipline and systems levels that will
address the technical challenges for two high-payoff NASA-unique
missions: Highly Reliable Reusable Launch Systems and High Mass Mars
Entry Systems.
Cutting-edge hypersonics research for Highly Reliable Reusable Launch
Systems will enable sustained hypersonic flight through the atmosphere
and can help the Department of Defense achieve its goal of reaching
targets from the air with global reach, quick reaction, persistence, and
significant payload. The research focused on High Mass Mars Entry
Systems will result in the development of technologies and concepts that
can enable the safe and accurate delivery of large payloads to the
surface of Mars. This effort will facilitate the EDL phase of both human
and robotic planetary missions and is closely aligned with the long-term
goals of NASA's Vision for Space Exploration.
The project will focus its research on solving some of the hardest
challenges in hypersonics such as the development of materials for
airframe and propulsion applications that can withstand severe
temperatures; the development of predictive models for compressible
flow, turbulence, heating, ablation, and combustion; the creation of
advanced control techniques for vehicles that fly in the hypersonic flow
regime; and the generation of new experimental techniques that can be
used to validate our theoretical and computational models. In addition,
the project will work towards realizable propulsion systems that
integrate high-speed turbine engines and scramjets, and will tie
together all of the interactions among the airframe, inlet, nozzle, and
propulsion systems using a Physics-Based MDAO approach.
The following are ROA-2007 NRA awards for the Hypersonics Project, with the most recent listed first.
+ ROA-2007 Hypersonics Project NRA Awards (click to open and close panel)

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| McCormick |
Uncertainty Quantification and Propagation Methods and Tools for System Level Analysis |
The Boeing Company |
CA |
07/03/2008 |
$205,000 |
| Wakayama |
System-Level Optimization with Uncertainty |
The Boeing Company |
CA |
07/03/2008 |
$237,000 |
| Vogel |
Development of a Control-Relevant Hypersonic Vehicle Modeling, Analysis, and Design Environment |
Vibroacoustics Solutions, Inc. |
IA |
05/30/2008 |
$495,293 |
| Donohue |
Dual-Mode Scramjet Flameholding Operability Measurements |
UTRC |
CT |
05/08/2008 |
$272,220 |
| Collier |
Analysis Methods for Durable, All Weather, Multifunctional and Modular Light Weight Structure/TPS |
Collier Research and Development Corporation |
VA |
04/17/2008 |
$244,000 |
| Morscher |
Assessment of SiC-Based Composites and Thermal Protection System (TPS) Materials and Systems |
Ohio Aerospace Institute |
OH |
04/04/2008 |
$141,478 |
| Spradley |
Multidisciplinary Modeling Software for Analysis, Design and Optimization of HRRLS Vehicles |
ResearchSouth, Inc. |
AL |
04/03/2008 |
$200,000 |
| Bradley |
Flowpath Integration for TBCC and RBCC Propulsion Systems |
The Boeing Company |
CA |
03/12/2008 |
$384,088 |
| Gamble |
Turbine-Based Combined Cycle Dynamic Simulation Model Development Program |
SPIRITECH Advanced Products, Inc. |
FL |
02/09/2008 |
$364,703 |
| Charania |
Activity-Based Simulation of Hypersonic System Operability and Affordability |
SpaceWorks Engineering, Inc. (SEI) |
GA |
01/30/2008 |
$275,000 |
| Coon |
Durability Variation of Ceramic Matrix Composites using a Stochastic, Hierarchical Topology Model |
University of Wyoming |
WY |
01/25/2008 |
$65,000 |
| Tiliakos |
MEMS Ablation Recession Rate Sensor (MARRS) for Real-Time, In-Situ TPS Recession Measurements and Surface Temperature |
Alliant Techsystems Inc. |
NY |
01/17/2008 |
$194,000 |
| Luo |
Development of a regional structured and unstructured grid simulation methodology for propulsion system analysis |
North Carolina State University |
NC |
12/21/2007 |
$118,000 |
| Papadopoulos |
Optically-coupled Shear Sensing Elements for Hypersonic Environment |
Alliant Techsystems Inc. |
NY |
12/21/2007 |
$200,000 |
| DeJarnette |
Rapid Method for Computing Heating Rates on Hypersonic Vehicles Using Unstructured Grids |
North Carolina State University |
NC |
12/18/2007 |
$159,212 |
| Lele |
Multi-fidelity Simulations of Shock Wave Turbulent Boundary Layer Interaction in Hypersonic Flows |
Stanford University |
CA |
12/18/2007 |
$298,268 |
| Givi |
Large Eddy Simulation of Turbulent Combustion via the Filtered Density Function |
University of Pittsburgh |
PA |
12/18/2007 |
$266,881 |
| Sanders |
Mode Transitioning for a Dual-Flow Turbine-Based Combined Cycle Hypersonic Propulsion System |
TechLand Research, Inc. |
OH |
12/18/2007 |
$215,000 |
| Sayir |
Multifunctional High Temperature Thermoelectric Power Generator for Hypersonic Vehicle |
Case Western Reserve University |
OH |
12/18/2007 |
$200,000 |
| Singh |
Design and Development of Advanced Gas-Impermeable High-Temperature Tubing for CMC Heat Exchanger Applications by Ion Assisted, High Energy Electron Beam-Physical Vapor Deposition |
Pennsylvania State University |
PA |
12/16/2007 |
$337,868 |
| Cutler |
Dual-pump CARS - Interferometric Rayleigh Scattering Measurements in Supersonic Combusting Flows |
George Washington University |
DC |
12/16/2007 |
$193,429 |
| McNamara |
Aero-Servo-Thermo-Elastic-Propulsion Modeling and Uncertainty Characterization for the Guidance, Navigation, and Control of Highly Reliable Reusable Launch Systems |
Ohio State University |
OH |
12/16/2007 |
$426,000 |
| Goldstein |
Modeling Non-equilibrium Flow Around Small Surface Irregularities Below a Hypersonic Boundary Layer |
University of Texas |
TX |
12/15/2007 |
$91,620 |
| Yungster |
Analysis of Unsteady Rocket-Based Combined-Cycle Propulsion Concepts |
Ohio Aerospace Institute |
OH |
12/15/2007 |
$181,441 |
| Miller |
Demonstration of a 3000F Composite Structure TPS |
Steve Miller & Associates Research |
VA |
12/15/2007 |
|
| Perepezko |
Synthesis and Design of Compatible Structures and Coatings for Robust TPS Applications in Hypersonics |
University of Wisconsin |
WI |
12/14/2007 |
$231,000 |
| Candler |
Advanced Simulation Tools for Hypersonic Flows |
University of Minnesota |
MN |
12/11/2007 |
$434,000 |
| Tolson |
Statistical Methods for Intelligent Data Integration (SMIDI) |
North Carolina State University |
NC |
12/11/2007 |
$172,000 |
| Hyers |
A Comprehensive Review of High-Temperature Sensing for Hypersonic Vehicles |
University of Massachusetts |
MA |
12/11/2007 |
$97,000 |
| Kim |
A Numerical Study of Turbulence Physics in Hypersonic Boundary Layers |
University of California, Los Angeles |
CA |
12/11/2007 |
$207,000 |
| Raman |
A Joint Computational/Experimental Program to Develop Predictive Turbulent Combustion Models for High-Speed Flows |
University of Texas |
TX |
12/10/2007 |
$287,466 |
| Mahadevan |
Uncertainty Quantification and Propagation Using Variable Fidelity Multidisciplinary and Probabilistic Analyses |
Vanderbilt University |
TN |
12/04/2007 |
$294,000 |
| Girimaji |
Development and Validation of High Fidelity RANS and Multi-Resolution Turbulence Models for Hypersonic Turbulent Combustion |
Texas A&M University |
TX |
12/04/2007 |
$204,435 |
| Haftka |
Uncertainty Propagation in the Analysis and Design of Integrated Thermal Protection System |
University of Florida |
FL |
11/30/2007 |
$165,845 |
| Smits |
Experiments on Impulses in Roughness, Transpiration and Heat Transfer in Supersonic and Hypersonic Turbulent Boundary Layers |
Princeton University |
NJ |
11/30/2007 |
$262,000 |

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

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Magaldi |
NDE and Damage Characterization of CMC Materials |
Hyper-Therm High Temperature Composites, Inc. |
CA |
02/28/2007 |
$149,000 |
| Cuneo |
Test Method Development for Use in the Analysis of Ceramic Matrix Composites in Advanced Structural and Thermal Protection System Hypersonic Applications |
Southern Research Institute |
AL |
02/27/2007 |
$174,000 |
| Vogel |
FADS-based Reconfigurable Control and Health Monitoring for Hypersonic Vehicles |
Vibroacoustics Solutions Inc. |
IA |
01/31/2007 |
$201,000 |
| Hamner |
Adaptation of Temperature and Pressure Sensitive Paint Technology for Basic Hypersonic Research |
LeaTech, LLC |
MA |
01/31/2007 |
$92,000 |
| Sullivan |
Integrated Durability Model for Ceramic Matrix Composite Components |
Materials Research & Design Inc. |
PA |
01/31/2007 |
$150,000 |
| Adamovich |
Nonequilibrium ignition and flame holding in high speed reacting flows |
Ohio State University |
OH |
01/30/2007 |
$170,000 |
| Lempert |
Development of MHz frame rate optical diagnostics for hypersonic ground test facilities |
Ohio State University |
OH |
01/30/2007 |
$244,000 |
| Przekop |
Probabilistic Analysis and Design Tools for High-Cycle Fatigue Resistant Hypersonic Vehicle Structures |
National Institute Of Aerospace Associates |
VA |
01/30/2007 |
$98,000 |
| Levin |
Coupled nonequilibrium flow, energy and radiation transport of hyper planetary entry |
Penn State University |
PA |
01/29/2007 |
$198,000 |
| Cutler |
Simultaneous Dual-broadband CARS and Interferometric Rayleigh Scattering |
The George Washington University |
DC |
01/26/2007 |
$256,000 |
| MacLean |
Measuring Wake Flows on Capsule Bodies |
CALSPAN-UB Research Center, Inc. |
NY |
01/26/2007 |
$171,000 |
| Santoro |
Performance Studies of the Ejector Mode of an Unsteady Pulse Detonation RBCC Engine |
Penn State University |
PA |
01/26/2007 |
$220,000 |
| Zhigilei |
Multiscale Computational Model for Multifunctional Nanocomposite Ablator Materials |
University of Virginia |
VA |
01/26/2007 |
$208,000 |
| Shaqfeh |
High Fidelity Simulations Tools for Space Exploration Vehicles |
Leland Stanford Junior University |
CA |
01/25/2007 |
$200,000 |
| Huo |
Chemical reaction and electron-impact excitation rates for direct numerical simulations and radiation transport modeling in the hypersonic regime |
HUO Consulting LLC |
CA |
01/25/2007 |
$114,000 |
| Hanson |
Hypersonic Mass-flux Sensing with Fiber-Coupled Tunable Diode Lasers for Ground Test Applications and Flight Evaluation |
Leland Stanford Junior University |
CA |
01/25/2007 |
$150,000 |
| Schneider |
Towards Mechanism-Based Models for Laminar-Turbulent Transition on a Representative Airbreathing Forebody: Mach-6 Quiet-Tunnel Experiments |
Purdue University |
ID |
01/25/2007 |
$100,000 |
| Jaberi |
A high fidelity model for numerical simulation of complex combustion and propulsion systems |
Michigan State University |
MI |
01/25/2007 |
$155,000 |
| Rodriguez |
Robust Hierarchical Control (Hi-C) for Future Hypersonic Vehicles with Aero-Thermo-Elastic-Propulsion Interaction |
Arizona State University |
AZ |
01/23/2007 |
$189,000 |
| Lind |
Multi-Loop Adaptive Control of Aerothermoelastic Dynamics |
University of Florida |
FL |
01/23/2007 |
$205,000 |
| Powers |
Advanced Multi-Scale Computational Methods for Hypersonic Propulsion |
University of Notre Dame DU LAC |
ID |
01/23/2007 |
$116,000 |
| Annaswamy |
Adaptive Robust Control for Hyp Vehicles (ARCH) |
Massachusetts Institute of Technology |
MA |
01/23/2007 |
$177,000 |
| Wu |
Reconfigurable robust gain-scheduled control for air-breathing hypersonic vehicles |
North Carolina State University |
NC |
01/23/2007 |
$157,000 |
| McDaniel |
Combustion Efficiency Measurement for Ground Test and Basic Hypersonic Research |
University of Virginia |
VA |
01/23/2007 |
$199,000 |
| Holton |
Protected, High Temperature Optical Fiber Sensors, Gauge Elements and Systems |
Virginia Polytechnic Institute & State University |
VA |
01/23/2007 |
$157,000 |
| Chelliah |
Reduced Reaction Models for Hypersonic Reacting Flow Simulations: Model Development and Validation Study |
University of Virginia |
VA |
01/23/2007 |
$144,000 |
| Goyne |
Test Media Effects on DMSJ Mode-Transition |
University of Virginia |
VA |
01/20/2007 |
$225,000 |
| Eldredge |
Numerical Investigations of Transitional and Turbulent Flow Physics in Hypersonic Boundary Layers |
University of California |
CA |
01/19/2007 |
$150,000 |
| Yang |
Low-Cost Manufacturing of C/ZrC Composites using Melt Infiltration/Reaction Approach for Ultrahigh Temperature TPS Applications |
University of California |
CA |
01/19/2007 |
$150,000 |
| Candler |
Advanced Aerothermodynamics Simulation Tools for HMMES Design and Optimization |
University of Minnesota |
MN |
01/19/2007 |
$170,000 |
| Xu |
Adaptive Identification and Control for Nonlinear Aerospace Systems by Multi-Parameter Regularization |
Syracuse University |
NY |
01/19/2007 |
$103,000 |
| Bhattacharya |
Robust Adaptive Guidance for High Mass Entry, Descent and Landing at Mars |
Texas Engineering Experiment Station |
TX |
01/19/2007 |
$175,000 |
| Mavriplis |
High Order Spatial and Temporal Methods for Simulation and Sensitivity Analysis of High-Speed Flows |
University of Wyoming |
WY |
01/19/2007 |
$150,000 |
| Edwards |
Development of Hybrid Large-Eddy / Reynolds-Averaged Navier-Stokes Methods for High-Speed Internal Flows |
North Carolina State University |
NC |
01/17/2007 |
$170,000 |
| Mangalam |
High-Sensitivity Heat Flux Gage for Calibrated Heat Transfer Measurements |
TAO Systems Integration, Inc. |
VA |
01/17/2007 |
$198,000 |
| Legzdina |
Optimization of Creep and Fatigue Resistance of Near Alpha Titanium alloys by Utilizing Beta Processing Route |
Honeywell International, Inc. |
AZ |
01/09/2007 |
$120,000 |
| Dunfey |
Design, Fabrication, and Testing of Load-Bearing TPS |
Materials Research & Design |
PA |
12/27/2006 |
$150,000 |

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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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