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Subsonic Rotary Wing Project
The goal of the Subsonic Rotary Wing project is to conduct long-term,
cutting-edge research in the core competencies of the subsonic rotary
wing regime, thereby producing knowledge, data, capabilities,
technologies, and design tools at the foundational, discipline,
multidiscipline and systems levels that will enable improved prediction
methods and technologies for lower noise, lower emissions, and higher
performance for rotary wing aircraft. Higher performance includes
improved speed, range, payload capacity, propulsion efficiency, and
control systems for safe operations. Advances in physics-based
prediction capability will ultimately lead to a more robust ability to
develop rotorcraft vehicles that fly as designed.
The specific objectives of the research are driven by five key technical
challenge areas: power transmission and generation; control theory and
information processing and modeling; fluid mechanics, dynamics, and
aero-structural coupling; acoustics physics; and solid mechanics and
advanced materials. These technical challenges are relevant to a broad
range of industry and government programs, inherently force the
integration of multiple disciplines, and involve technical issues that
are beyond the reach of current prediction tools. Each of the technical
challenges brings together the analytical methods and experimental
validation data that are required to advance the state-of-the-art in a
multi-discipline environment. Innovative solutions to these technical
challenges, coupled with the increased ability to predict with certainty
the solutions, will drive breakthrough technology for the rotorcraft
industry.
The following are ROA-2007 NRA awards for the SRW Project, with the most recent listed first.
+ ROA-2007 SRW Project NRA Awards (click to open and close panel)

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Hambric |
Rotorcraft Transmission Noise Path Model, Including Distributed Fluid Film Bearing Impedance Modeling |
Pennsylvania State University |
PA |
09/29/2008 |
$207,215 |
| Parker |
Vibration Propagation of Gear Dynamics in a Gear-Bearing-Housing System using Mathematical Modeling and Finite Element Analysis |
Ohio State University |
OH |
09/24/2008 |
$117,380 |
| Van Slooten |
High Efficiency Centrifugal Compressors for Rotorcraft Applications |
United Technologies Corporation |
CT |
09/22/2008 |
$782,000 |
| Fidell |
Research Plan for Human Response to Low-Frequency Rotor Noise |
Fidell Associates Inc |
|
08/20/2008 |
$154,500 |
| Sharp |
A Research Plan to Determine the Effects of Low-Frequency Noise on Humans |
Wyle Laboratories, Inc. |
VA |
08/20/2008 |
$170,146 |
| Narducci |
Coupled CFD/CSD/Icing Analysis for Rotorcraft in Forward Flight |
The Boeing Company |
CA |
08/15/2008 |
$191,000 |
| Noack |
High Resolution CFD Analysis of Rotorcraft Rotor Icing |
Pennsylvania State University |
PA |
08/02/2008 |
$186,590 |
| Sankar |
Development of Methodologies for Coupling Ice Accretion Models with Rotary Wing Aeromechanics |
Georgia Tech Research Corporation |
GA |
07/25/2008 |
$199,495 |

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

| PI Last Name |
Title |
Organization |
State |
Award Date |
Year 1 Amount |
| Mitchell |
Determining Effects of Time-Varying Rotorcraft Dynamics on Pilot Control |
Hoh Aeronautics |
CA |
09/25/2007 |
$182,900 |
| Noack |
Innovative Overset Grid Connectivity Software for Unstructured Rotorcraft Simulations |
Penn State |
PA |
09/21/2007 |
$325,000 |
| Baeder |
Innovative Parallel Framework for Coupling Advanced Rotorcraft Aeromechanic Simulations |
University of Maryland |
MD |
09/17/2007 |
$446,000 |
| Sankaran |
Unified Computational Platform for CFD and CSD for Rotorcraft Aeromechanics |
UC |
CA |
09/10/2007 |
$200,000 |
| Orr |
Framework for Multidisciplinary Analysis, Design, and Optimization with High-Fidelity Analysis Tools |
Boeing |
PA |
09/06/2007 |
$436,000 |
| Prasad |
Flight Mechanics and Control Oriented Modeling of Next Generation On-Blade Control Concepts |
GTRC |
GA |
08/29/2007 |
$176,000 |
| Hess |
Development and Validation of Multi-Axis Pilot Models for Rotorcraft With Time-Varying Dynamics and Biodynamic Interface |
UC Davis |
CA |
08/16/2007 |
$60,000 |
| Carpino |
Thermal Effects in Gas Lubricated Foil Journal Bearing Performance |
Penn State |
PA |
08/08/2007 |
$148,000 |
| San Andres |
Prediction of Foil Bearing Perfomrance: A computational Model Anchored to Test Data |
Texas Eng Exp Station |
TX |
08/08/2007 |
$159,000 |
| Smith |
Innovative Strategies for Rotary-Wing Coupled Aeroelastic Simulations |
GTRC |
GA |
08/07/2007 |
$146,000 |
| Celi |
Control-Oriented Modeling of Free Vortex Wakes |
University of Maryland |
MD |
07/31/2007 |
$173,000 |
| Wilkerson |
Aircraft System Analysis of Technology Benefits to Civil Transport Rotorcraft |
Boeing |
PA |
|
$420,000 |
| Anusonti-Inthra |
Integrated Algorithms for High-Fidelity Rotorcraft Aeromechanics Predictions within CFD/CSD-Coupled Frameworks |
National Institute of Aerospace Associates |
VA |
02/05/2007 |
$130,000 |
| Liu |
Multidisciplinary Computational Tool for Accurate and Efficient Rotorcraft Noise Prediction (MUTE) |
National Institute of Aerospace Associates |
VA |
02/05/2007 |
$175,000 |
| Chang |
Crashworthiness Analysis of Composite Structures |
Leland Stanford Junior University |
CA |
01/27/2007 |
$122,507 |
| Chopra |
Detailed Performance, Wakes, Pressures and Loads for High Speed Single and Coaxial Rotors |
University of Maryland - College Park |
MD |
01/25/2007 |
$310,001 |
| Schmitz |
Fundamental Acoustic Design Tool Development and Validation for Rotorcraft External Noise |
University of Maryland - College Park |
MD |
01/25/2007 |
$250,390 |
| Schmitz |
A Helicopter Tip-Path-Plane Measurement System Using an Optics-Based Method |
University of, College Park Maryland |
MD |
01/25/2007 |
$178,527 |
| Ruzzene |
Control of Vibration Transmission and Interior Noise Radiation of Composite Shells with Embedded Passive and Active Periodicity |
Georgia Tech Research Corp. |
GA |
01/12/2007 |
$100,199 |
| Vlahopoulos |
EFEA developments for metallic/composite rotorcraft configurations |
University of Michigan |
MI |
01/12/2007 |
$150,000 |
| Tabakoff |
A Study of Thermal Barrier Coating Erosion in Rotorcraft Engine |
University of Cincinnati |
OH |
01/12/2007 |
$177,000 |
| Kunz |
High Fidelity CFD Analysis & Validation of Rotorcraft Gear Box Aerodynamics Under Operational & Oil-Out Conditions |
Pennsylvania State University |
PA |
01/09/2007 |
$200,000 |
| Wang |
Comprehensive Modeling & Analysis of Rotorcraft Variable Speed Propulsion System with Coupled Engine/Transmission/ Rotor Dynamics |
Pennsylvania State University |
PA |
12/21/2006 |
$221,000 |
| Glezer |
Combustion Powered Actuators (COMPACT) for Aerodynamic Flow Control on Rotorcraft Blades |
Georgia Tech Research Corp. |
GA |
12/21/2006 |
$210,274 |

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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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