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Targazyme, Inc.

Company Information
Address
2100 Palomar Airport Rd Ste 214-19
CARLSBAD, CA 92011-4402
United States


https://www.targazyme.com
Information

UEI: NJG4X7NZ4BM1

# of Employees: 5
Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: Yes

Award Charts




Award Listing

  • Record 1 TO 27

  1. A METHOD TO PREDICT SEPARATION DELAY ON AIRFOILS DUE TO VORTEX GENERATORS

    Amount: $70,000.00

    N/A

    SBIRPhase I1996National Aeronautics and Space Administration

  2. Prediction Method for Hydrodynamic Problems of Two Bodies Operating in Close Proximity

    Amount: $744,171.00

    The Navy's plan to launch and retrieve Unmanned Undersea Vehicles (UUVs) from submarines will require precise control of the UUV when it is in close proximity to the submarine hull. The hydrodynamic f ...

    SBIRPhase II1995Department of Defense Navy

  3. Multidisciplinary Design Opimization (MDO)

    Amount: $100,000.00

    N/A

    SBIRPhase I1995Department of Defense Air Force

  4. Unsteady Aerodynamic And Aeroelastic Simulation Using Panel Methods Coupled To A Finite Element Structures Method

    Amount: $70,000.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration

  5. Prediction Method for Hydrodynamic Problems of Two Bodies Operating in Close Proximity

    Amount: $70,000.00

    N/A

    SBIRPhase I1994Department of Defense Navy

  6. A NOVEL COUPLING TECHNIQUE FOR SOLVING THE EULER EQUATIONS OVER COMPLETE AIRCRAFT

    Amount: $49,732.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration

  7. A NOVEL POTENTIAL/VISCOUS FLOW COUPLING TECHNIQUE FOR COMPUTING HELICOPTER FLOW FIELDS

    Amount: $1,492,497.00

    BECAUSE OF THE COMPLEXITY OF THE HELICOPTER FLOW FIELD, A ZONAL METHOD OF ANALYSIS OF COMPUTATIONAL AERODYNAMICS IS REQUIRED. IN THIS RESEARCH, A NEW PROCEDURE FOR COUPLING POTENTIAL AND VISCOUS FLOW ...

    SBIRPhase II1990National Aeronautics and Space Administration

  8. A NOVEL POTENTIAL/VISCOUS FLOW COUPLING TECHNIQUE FOR COMPUTING HELICOPTER FLOW FIELDS

    Amount: $50,000.00

    N/A

    SBIRPhase I1989National Aeronautics and Space Administration

  9. DEVELOPMENT OF A PANEL METHOD FOR MODELING CONFIGURATIONS WITH UNSTEADY COMPONENT MOTIONS

    Amount: $338,000.00

    A PROGRAM OF STUDY IS PROPOSED WHICH WILL LEAD TO A PRACTICAL ANALYSIS CAPABLE OF CALCULATING THE FLOW AROUND AND THE LOADS ON CONFIGURATIONS WHERE ELEMENTS OF THE VEHICLE ARE IN MOTION RELATIVE TO EA ...

    SBIRPhase II1988Department of Defense Army

  10. A PREDICTION MODEL FOR ADVANCED LEADING-EDGE VORTEX FLOW CONTROL

    Amount: $110,000.00

    THE OBJECTIVE IS TO DEVELOP A TOOL FOR DESIGNING VORTEX FLAPS ON ADVANCED FIGHTER AIRCRAFT INCLUDING THE EFFECTS OF VISCOSITY. ANALYTICAL METHODS, INC. PROPOSES TO USE AN UNSTEADY TIME-STEPPING VERSIO ...

    SBIRPhase II1987Department of Defense Air Force
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