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Company Information:

Company Name:
Innovative Aerodynamic
Address:
534 Wythe Creek Road, Suite C
Poquoson, VA 23662
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
8
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 $429,249.00 6
SBIR Phase II $2,399,664.00 4

Award List:

Full-Chord Laminar Flow for GA Aircraft Wings with a Limited Suction

Award Year / Program / Phase:
1991 / SBIR / Phase I
Award Amount:
$50,000.00
Agency:
NASA
Principal Investigator:
Sally Viken , Aerospace Engineer
Abstract:
N/a

A User-Friendly Expert System for Airfoil Design and Boundary-Layer Stability Analysis

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Sally Viken
Abstract:
N/a

Full-Chord Laminar Flow for GA Aircraft Wings with a Limited Suction Region

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$70,000.00
Agency:
NASA
Principal Investigator:
Sally Viken
Abstract:
N/a

Full-Chord Laminar Flow for GA Aircraft Wings with a Limited Suction Region

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$600,000.00
Agency:
NASA
Principal Investigator:
Sally Viken
Abstract:
The perennial demand in the GA market for more speed can be metwithout power increases by achieving extensive runs of laminarflow. The use of full chord laminar flow can provide an eightfold decrease in wing parasite drag and as much as a 35%reductio

A User-Friendly Expert System for Airfoil Design and Boundary-Layer Stability Analysis

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$599,664.00
Agency:
NASA
Principal Investigator:
Sally Viken
Abstract:
The quest for performance, fuel efficiency, range and speed inthe current global economic environment, has sparked a renewedinterest in designing and analyzing lamianar flow wings forairplanes. Currently, the capability to design and analyzelaminar f

Full-Chord Laminar Flow for GA Aircraft Wings with a Limited Suction

Award Year / Program / Phase:
1995 / SBIR / Phase II
Award Amount:
$600,000.00
Agency:
NASA
Principal Investigator:
Sally Viken , Aerospace Engineer
Abstract:
N/a

Aircraft Drag Reduction Using Distributed Suction And Adaptive Control Techniques

Award Year / Program / Phase:
1995 / SBIR / Phase I
Award Amount:
$69,633.00
Agency:
NASA
Principal Investigator:
Sally A. Viken , Aerospace Engineer
Abstract:
N/a

Aircraft Drag Reduction Using Distributed Suction And Adaptive Control Techniques

Award Year / Program / Phase:
1996 / SBIR / Phase II
Award Amount:
$600,000.00
Agency:
NASA
Principal Investigator:
Sally A. Viken , Aerospace Engineer
Abstract:
N/a

Advanced High-Lift Systems To Enhance Performance And Utility Of Existing And New Ga Aircraft

Award Year / Program / Phase:
1997 / SBIR / Phase I
Award Amount:
$69,626.00
Agency:
NASA
Principal Investigator:
Sally Viken , RESEARCH SCIENTIST
Abstract:
N/a

Portable Electromagnetic Diagnostic Tool for Nondestructive Evaluation System

Award Year / Program / Phase:
1998 / SBIR / Phase I
Award Amount:
$99,990.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Dr. M.d. Deshpande
Abstract:
Composite materials are being used in many practical applications such as aircraft, automobiles, spacecraft etc. for flghtweight. However, successful use of composite materials in these applications depends upon customer's ability to determine their properties and detecting volumetric or surface… More