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Company Information:

Company Name:
Frendi Research Corporation
Address:
7561 Wall Triana Highway
Madison, AL 35757-8327
Phone:
(256) 824-7206
URL:
N/A
EIN:
203898184
DUNS:
118538086
Number of Employees:
2
Woman-Owned?:
Yes
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 $210,180.00 3

Award List:

Prediction and Control of the Vibroacoustic Environment During a Launch Sequence

Award Year / Program / Phase:
2006 / SBIR / Phase I
Award Amount:
$69,930.00
Agency:
NASA
Principal Investigator:
Kader Frendi, Principal Investigator
Abstract:
The complexity of the current launch platforms makes their maintenance and operation very costly. In order to successfully design the next generation platforms, it is necessary to understand the complex, multi-disciplinary environments that exists during a launch sequence. The proposed research and… More

A High Order Accuracy Computational Tool for Unsteady Turbulent Flows and Acoustics

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$69,675.00
Agency:
NASA
Principal Investigator:
Kader Frendi, Principal Investigator
Abstract:
The main objective of this research effort is to develop a higher order unsteady turbulent flow solver based on the FDV method, and to exploit its attributes of spanning the whole Mach number range.The well known advantages of the implicit FEM will be inherited along with robust boundary conditions… More

Computations of Separated High-Enthalpy Hypersonic Flows: Development of RANS and Variable-Resolution PANS Approaches

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$70,575.00
Agency:
NASA
Principal Investigator:
Kader Frendi, Principal Investigator
Abstract:
We propose the development of a high fidelity computational approach for unsteady calculations of strongly separated non-equilibrium high-enthalpy hypersonic flows. The goal is to integrate the now proven partially-averaged Navier-Stokes (PANS) method for unsteady flow simulations with the most… More