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Company Information:

Company Name:
Innovative Technology Applications Co.
Address:
P.O. Box 6971
Chesterfield, MO 63006-6971
Phone:
N/A
URL:
N/A
EIN:
431867210
DUNS:
126752018
Number of Employees:
5
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $474,852.00 4

Award List:

Shock Generation and Control Using DBD Plasma Actuators

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$99,999.00
Agency:
NASA
Principal Investigator:
Mehul P. Patel, Principal Investigator
Abstract:
Shock-wave/boundary-layer interactions (SWBLI) pose challenges to aeronautical engineers because they create regions of adverse pressure gradients as a result of the discontinuous change in conditions across the shock. This shock-induced pressure gradient is a common factor for both flow separation… More

Extension of the Eddy Dissipation Concept for Improved Low-Cost Turbulence-Chemistry Interaction Modeling

Award Year / Program / Phase:
2012 / SBIR / Phase I
Award Amount:
$124,855.00
Agency:
NASA
Principal Investigator:
Chris C. Nelson, Principal Investigator
Abstract:
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… More

Plasma Fairings for Quieting Aircraft Landing Gear Noise

Award Year / Program / Phase:
2013 / SBIR / Phase I
Award Amount:
$124,999.00
Agency:
NASA
Principal Investigator:
Chris C. Nelson, Principal Investigator
Abstract:
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… More

Identification of Landing Gear Aeroacoustic Noise Sources with the Synthetic Array Technique

Award Year / Program / Phase:
2013 / SBIR / Phase I
Award Amount:
$124,999.00
Agency:
NASA
Principal Investigator:
Chris Nelson, Principal Investigator
Abstract:
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,… More