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VIGYAN INC

Company Information
Address
30 RESEARCH DR
HAMPTON, VA 23666-1325
United States
Information

UEI: FJM8WZ8EF8K6

# of Employees: 25
Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: Yes

Woman Owned: No

Award Charts




Award Listing

  • Record 1 TO 38

  1. Full Scale Development and Demonstration of an Automated Active Damper Sting

    Amount: $748,284.00

    Unwanted vibration of heavy, sting-mounted cantilevered models is an ongoing issue for wind tunnel facilities. As noted in this SBIR topic solicitation, “unsteady flow generated on models can re ...

    SBIRPhase II2019Department of Defense Air Force

  2. Development and Feasibility Demonstration of an Automated Active Damper Sting

    Amount: $149,875.00

    Unwanted vibration of heavy, sting-mounted, cantilevered models is an ongoing issue for wind tunnel facilities. Unsteady flow generated on models can result in vibration and oscillation of the model s ...

    SBIRPhase I2017Department of Defense Air Force

  3. Identification of Traumatic Brain Injury using Abnormal Speech Audio Processing (TBI-ASAP)

    Amount: $99,965.00

    Traumatic Brain Injury (TBI) is a constant risk for soldiers in the military work and combat environment. From vehicle accidents to explosions, a soldier can experience TBI over a range of conditions ...

    SBIRPhase I2015Department of Defense Army

  4. Development of a "Digital Bridge" Thermal Anemometer for Turbulence Measurements

    Amount: $749,996.00

    Thermal anemometry (a.k.a. hot-wire anemometry) has been a key experimental technique in fluid mechanics for many decades. Due to the small physical size and high frequency response of the sensors (re ...

    SBIRPhase II2015National Aeronautics and Space Administration

  5. Development of a "Digital Bridge" Thermal Anemometer for Turbulence Measurements

    Amount: $125,000.00

    Thermal anemometry (a.k.a. hot-wire anemometry) has been a key experimental technique in fluid mechanics for many decades. Due to the small physical size and high frequency response of the sensors (re ...

    SBIRPhase I2014National Aeronautics and Space Administration

  6. Wind Tunnel Active Vibration Reduction System (WTAVRS)

    Amount: $99,874.00

    During wind tunnel testing of scaled aerodynamic models, the most critical measuring device is the internal strain gage balance. Modern internal balances are intricate and precise devices, which resol ...

    SBIRPhase I2005Department of Defense Air Force

  7. Low-Cost Piston Engine Health Monitoring and Control System for General Aviation

    Amount: $69,699.00

    N/A

    SBIRPhase I1998National Aeronautics and Space Administration

  8. A Novel Pneumatic Vortex Control Technique For Lift And Maneuverability Enhancement Of Highly-Swept Configurations

    Amount: $69,975.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration

  9. Vortex Flap Improvements for Enhanced Low-Speed Aerodynamics of Supersonic-Cruise Aircraft

    Amount: $70,000.00

    Leading edge vortex flap modifications are proposed for improvedlow-speed lift and L/D characteristics of supersonic cruiseaircraft. The aim is to increase the vortex-lift potential inaddition to gene ...

    SBIRPhase I1994National Aeronautics and Space Administration

  10. Active Flow-Control Concepts for Stall Alleviation and Post-Stall Lift Improvement of Vortex Dominated Fighter Configuration

    Amount: $60,099.00

    It is proposed to experimentally explore two active separation-control concepts aimed at stall alleviation and maximum-lift improvement on generic, vortex-dominated fighter configurations. The concept ...

    SBIRPhase I1993Department of Defense Air Force
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