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ARMD NRA AWARDS: FUNDAMENTAL AERONAUTICS PROGRAM
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


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




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


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