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Company Information:

Company Name:
Optimal Solutions Software, LLC
Address:
PO Box 2427
Idaho Falls, ID
Phone:
(208) 521-4660
URL:
N/A
EIN:
820529885
DUNS:
12832130
Number of Employees:
4
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 $168,442.00 2
SBIR Phase II $599,979.00 1
STTR Phase I $79,634.00 1

Award List:

Efficient CFD-Based Aerodynamic Shape Optimization

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$99,978.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Mark Landon
Abstract:
The overall objective of this work is to develop a general-purpose CFD-based, shape optimization tool for robust and efficient aerodynamic shape optimization. Shape optimization is a technology where design optimization algorithms are coupled with geometry/shape deformation tools and engineering… More

Automated Computational Fluid Dynamics Design With Shape Optimization

Award Year / Program / Phase:
2004 / SBIR / Phase I
Award Amount:
$68,464.00
Agency:
NASA
Principal Investigator:
Ernest C. Perry, Principal Investigator
Abstract:
Computational fluid dynamics (CFD) is used as an analysis tool to help the designer gain greater understanding of the fluid flow phenomena involved in the components being designed. The next step in the design process is to modify the design to improve the componentys performance, typically… More

Automated Computational Fluid Dynamics Design With Shape Optimization

Award Year / Program / Phase:
2005 / SBIR / Phase II
Award Amount:
$599,979.00
Agency:
NASA
Principal Investigator:
Abstract:
Computational fluid dynamics (CFD) is used as an analysis tool to help the designer gain greater understanding of the fluid flow phenomena involved in the components being designed. The next step in the design process is to modify the design to improve the components performance, typically performed… More

Modeling of Integrally Bladed Rotor (IBR) Blends

Award Year / Program / Phase:
2013 / STTR / Phase I
Award Amount:
$79,634.00
Agency:
DOD
Principal Investigator:
Mark Landon, Chief Technical Officer – (208) 521-4660
Research Institution:
University of Michigan
RI Contact:
Patrick J. Woods
Abstract:
The overall goal of this Phase I project is to show the feasibility of using state-of-the-art parameterization tools for shape changes (i.e., volumetric deformation/morphing provided by Sculptor) coupled with a fast FEA tool (i.e., the MAX method) to quickly calculate the dynamic response of the… More