| Last Name | Name | Awards | Contact | |
|---|---|---|---|---|
| Hazinski | Ms. Nancy A. Hazinski | 4 | Message | |
| Morris | Dr. Philip J Morris | 3 | Message | |
| Patel | Mehul Patel | 5 | Message | |
| Rennie | Mark Rennie | 4 | Message | |
| Cain | Dr. Alan B. Cain | 25 | Message | |
| Nelson | Dr. Chris C. Nelson | 10 | Message |
Phase 2 SBIR
This Phase II SBIR project deals with advancing the design, development, and testing of an innovative drag reduction concept named ?Smart Longitudinal Instability Prevention via Plasma Surface? using a new revolutionary plasma actuator technology developed at the University of Notre Dame (UND). During Phase I, Innovative Technology Applications ...
Phase 1 SBIR
Fuel costs have historically been the largest single cost associated with aircraft operations; improved efficiency therefore translates directly to the bottom line. The worldwide aviation industry is a significant emitter of carbon dioxide and other greenhouse gases; the International Civil Aviation Organization puts it at 2% of the global anth...
Phase 1 SBIR
ABSTRACT:Innovative Technology Applications Company, LLC proposes the development of an analytical tool that predicts jet noise and engine performance for current and future generations of supersonic two- and three-stream engines. ?The goal is to provide robust and reliable noise predictions in minutes that can be used for design optimization. ?...
Phase 1 SBIR
ITAC and its partners propose to develop and demonstrate a computational technology and methodology tool for the concurrent automated shaping of aft airframe and nozzle geometries to reduce tactical aircraft jet noise without any performance penalties. The proposed technologies will lead to an integrated tool which inherently maintains critical ...
Phase 2 SBIR
This Phase II SBIR project deals with the design, development, and testing of a "Plasma Fairing" to reduce noise on the Gulfstream G550 landing gear. The plasma fairing will use single dielectric barrier discharge (SDBD) plasma actuators to reduce flow- separations and impingement around the landing gear, which are the dominant sources of landi...
Phase 2 STTR
Institution: University of Notre Dame
ABSTRACT: Under this Small Business Technology Transfer (STTR) program, Innovative Technology Applications Company (ITAC), LLC and the University of Notre Dame (UND) are working to develop new optical instruments that will enable nonintrusive, off-body measurements of flow parameters in hypersonic flight. The two concepts under development by t...
Phase 1 SBIR
A major component of airframe noise for commercial transport aircraft is the deployed landing gear. The noise from the gear originates due to complex, unsteady bluff body flow separation from gear components and the subsequent multiple interactions of unsteady wakes with downstream undercarriage elements. The object of this SBIR effort is to d...
Phase 1 SBIR
In this program, Innovative Technology Applications Company (ITAC), LLC and collaborators propose to advance "synthetic phased array" technology to improve understanding of noise from landing gear. The technology, initially developed in a previous NASA SBIR project for trailing edge noise, will be applied to improve beamforming analysis methods,...
Phase 1 SBIR
The one CFD modeling area that has remained the most challenging, yet most critical to the success of integrated propulsion system simulations, is turbulence modeling. There is a need to develop mid-level CFD models for the interaction of turbulence and chemical reactions that give superior results to the simple models (e.g., Magnussen's Eddy Di...
Phase 2 STTR
Institution: University of Notre Dame
ABSTRACT: The objective of the Phase II effort is to extend the mathematical model investigated in the Phase I to include wind speed as well as temperature modeling, continue its development for a University of Notre Dame Wind Tunnel Facility, and demonstrate utility by adopting the model to a government facility specified by AFOSR. Specifically...
