TTC Technologies, Inc.

P. O. Box 1527
Stony Brook, NY 11790
http://www.ttctech.com
12 Employees

SBIR Award Summary

Total Number of Awards 6
Total Value of Awards $1.95MM
First Award Date 12/14/07
Most Recent Award Date 07/15/10

Key Personnel

Last Name Name Awards Contact
Alabi Dr. Ken Alabi 4 Message
Cai Dr. Xiaodan Cai 2
Ladeinde Foluso Ladeinde 1 Message

6 Awards Won

Phase 1 STTR

Institution: The Ohio State University

Agency: Air Force
Topic: AF09-BT10
Budget: 07/15/10 - 04/15/11

A computational and experimental research program is proposed to develop and validate a high-fidelity 3D non-equilibrium magnetohydrodynamic (MHD) plasma compressible flow code for advanced aerospace applications. The code will incorporate a physics-based kinetic model of air plasma with non-equilibrium conductivity sustained by an externally ap...

Phase 2 SBIR

Agency: Navy
Topic: N07-173
Budget: 08/27/09 - 02/27/11

The development of optimal engine exhaust noise reduction technology for tactical aircraft continues to rely heavily on laboratory-scale testing due to the absence of appropriate modeling and analysis capability. Thus, concept identification relies largely on engineering intuition, ad hoc reasoning, and exhaustive parametric testing. Another obs...

Phase 2 SBIR

Agency: Air Force
Topic: AF073-060
Budget: 03/04/09 - 06/04/11

Several high-fidelity computational schemes and turbulence-combustion interaction models, including the option for high-order spatial and temporal calculations, are proposed to significantly improve the accuracy and turnaround time for practical scramjet engine design and performance analysis. The proposed enhancements of existing tools, such as...

Phase 1 SBIR

Agency: Navy
Topic: N07-173
Budget: 01/10/08 - 03/16/09

The absence of a comprehensive, integrated aerodynamic/aero-acoustic modeling and analysis framework represents an impediment to achieving significant noise reduction within constraints imposed by the engine cycle, realistic geometry, and airframe. We close the gap by developing a suite of advanced, high fidelity nozzle performance and jet noise...

Phase 1 SBIR

Agency: Air Force
Topic: AF073-050
Budget: 12/17/07 - 09/17/08

An advanced software tool for heat exchanger (HEX) characterization and scaling for high-performance aircraft is proposed, with the objective of removing the limitations associated with the existing methods of analysis. In addition to supporting the conventional methods of analysis, which are based on the lumped approach, the proposed tool will ...

Phase 1 SBIR

Agency: Air Force
Topic: AF073-060
Budget: 12/14/07 - 09/14/08

Several high-fidelity computational schemes and turbulence-combustion interaction models, including the option for high-order spatial and temporal calculations, are proposed to significantly improve the accuracy and turnaround time for practical scramjet engine design and performance analysis. The proposed enhancements of existing tools, such as...