Cambridge Hydrodyn Inc

Company Information

Company Name
Cambridge Hydrodyn Inc
Address
P O Box 1403
Princeton, NJ, 08542 0140
Phone
1 609-683-1515
URL
n/a
DUNS
n/a
Number of Employees
n/a
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,132,364.00
19
SBIR Phase II
$3,568,667.00
9

Award List

  1. RENORMALIZATION GROUP FORMULATION OF TURBULENT TRANSPORT IN COMPLEX MEDIA

    Amount: $189,000.00

    RENORMALIZATION GROUP (RNG) METHODS ARE APPLIED TO THE DERIVATION OF TURBULENCE TRANSPORT MODELS FOR FLOWS WITH COMPLEX PHYSICS, LIKE TWO-PHASE FLOWS AND COMBUSTING FLOWS. THE RNG METHODS ARE ATTRACTI ...

    SBIR Phase II 1987 National Science Foundation
  2. NUMERICAL MODELLING OF MIXING AND CHEMICAL REACTIONS IN TURBULENT FLOWS

    Amount: $49,654.00

    WE SHALL DEVELOP METHODS TO SOLVE ONE OF THE CRITICAL PROBLEMS OF TURBULENCE MODELLING IN WHICH ALL TRADITIONALLY USED TURBULENCE MODELS FAIL, NAMELY MODELLING OF MIXING AND CHEMICAL REACTIONS IN COMP ...

    SBIR Phase I 1989 Air ForceDepartment of Defense
  3. COMPUTATIONAL MODEL OF PROJECTILE IMPACT INTO FUEL TANKS

    Amount: $49,902.00

    THE OBJECTIVE OF THIS WORK IS TO INVESTIGATE THE UTILITY OF COMPUTATIONAL FLUID DYNAMIC (CFD) MODELS TO SIMULATE REACTIONS WITHIN FLUID-FILLED TANKS IMPACTED BY WARHEAD FRAGMENTS. IN PHASE I, WE WILL ...

    SBIR Phase I 1989 Air ForceDepartment of Defense
  4. NUMERICAL MODELLING OF KINETICS-TURBULENCE INTERACTION IN HIGH MACH NUMBER FLOWS

    Amount: $195,000.00

    WE PROPOSE TO DEVELOP METHODS TO SOLVE ONE OF THE CRITICAL PROBLEMS OF TURBULENCE MODELLING INVOLVED IN HYPERSONIC FLOW IN WHICH ALL TRADITIONALLY USED TURBULENCE MODELS FAIL, NAMELY MODELLING OF KINE ...

    SBIR Phase II 1990 Air ForceDepartment of Defense
  5. NUMERICAL MODELLING OF TURBULENCE AND COMBUSTION PROCESSES IN STRONGLY SEPARATED, NON-STATIONARY FLOWS

    Amount: $395,000.00

    WE PROPOSE TO DEVELOP A THREE-DIMENSIONAL COMPUTER CODE INCORPORATING RENORMALIZATION-GROUP (RNG) BASED DIFFERENTIALTRANSPORT MODELS FOR TURBULENT HEAT, MASS, MOMENTUM TRANSFERAND COMBUSTION PROCESSES ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  6. COMPUTATIONAL DYNAMICS OF TWO-PHASE FLOWS

    Amount: $49,526.00

    THE RESEARCHERS PROPOSE TO DERIVE EQUATIONS OF MOTION FOR MULTI-PHASE FLUID FLOWS USING VARIOUS LEVELS OF COARSE-GRAINING ON THE MICROSCOPIC DYNAMICS AND THEREBY OBTAIN DYNAMICALLY CONSISTENT AND USEF ...

    SBIR Phase I 1989 National Science Foundation
  7. SLUGLESS MULTIPLE HIGH VELOCITY PULSE SHAPED CHARGE JETS

    Amount: $49,982.00

    THIS PROPOSAL IS TO APPLY COMPUTATIONAL FLUID DYNAMIC (CFD) SIMULATIONS TO DESIGN SLUGLESS HIGH VELOCITY PULSE SHAPED CHARGE WARHEADS FOR ARMOR PENETRATION. WE HVE DEVELOPED A NEW AND VERY NOVEL CODE ...

    SBIR Phase I 1990 ArmyDepartment of Defense
  8. SLUGLESS MULTIPLE HIGH VELOCITY PULSE SHAPED CHARGE JETS

    Amount: $49,982.00

    THIS PROPOSAL IS TO APPLY COMPUTATIONAL FLUID DYNAMIC (CFD) SIMULATIONS TO DESIGN SLUGLESS HIGH VELOCITY PULSE SHAPED CHARGE WARHEADS FOR ARMOR PENETRATION. WE HVE DEVELOPED A NEW AND VERY NOVEL CODE ...

    SBIR Phase I 1991 ArmyDepartment of Defense
  9. LARGE-EDDY SIMULATION OF COMBUSTION OF LIQUID FUEL ROCKETS

    Amount: $49,996.00

    THE DESIGN, OPTIMIZATION, SIMULATION, AND TESTING OF LIQUID-FUEL ROCKET ENGINES INVOLVES A WIDE VARIETY OF GEOMETRICALLY COMPLEX, UNSTEADY, TURBULENT, MULTIDIMENSIONALREACTIVE FLOW PROBLEMS. IN A HIGH ...

    SBIR Phase I 1991 National Aeronautics and Space Administration
  10. ADVANCED TURBOMACHINERY CFD DESIGN AND ANALYSIS PROGRAM

    Amount: $479,800.00

    COMPUTATIONAL FLUID DYNAMICS (CFD) TOOLS HAVE NOW DEVELOPED TO THE POINT WHERE THEY CAN BE RELIABLY USED FOR THE DESIGN,EVALUATION, AND ANALYSIS OF SUCH HIGH-PERFORMANCE GAS TURBINES AS THOSE USED IN ...

    SBIR Phase II 1992 National Aeronautics and Space Administration

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