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CONTINUUM DYNAMICS INC

Company Information
Address
34 LEXINGTON AVE
EWING, NJ 08618-2302
United States


http://www.continuum-dynamics.com

Information

UEI: DUE3E75K1MJ3

# of Employees: 25


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. VORTEX DYNAMICS FOR ROTORCRAFT INTERACTIONAL AERODYNAMICS

    Amount: $49,657.00

    N/A

    SBIRPhase I1987Department of Defense Army
  2. COMPUTER TECHNOLOGY TO EVALUATE AIRCRAFT VORTEX WAKE INTENSITY

    Amount: $296,012.00

    THERE DOES NOT EXIST TODAY A UNIFIED MEANS OF EVALUATING THE VORTEX INTENSITY BEHIND COMMERCIAL JET LINERS PRIOR TO PROTOTYPE DEVELOPMENT AND TESTING AT FULLSCALE. OVER THE PAST SEVERAL YEARS, DATA AN ...

    SBIRPhase II1985Department of Transportation
  3. UNDER IFR CONDITIONS, AIRPORT CAPACITY IS CURRENTLY LIMITED BY FAA SEPARATION STANDARDS BETWEEN AIRCRAFT.

    Amount: $49,859.00

    UNDER IFR CONDITIONS, AIRPORT CAPACITY IS CURRENTLY LIMITED BY FAA SEPARATION STANDARDS BETWEEN AIRCRAFT. THESE STANDARDS ARE SET TO AVOID A LANDING ENCOUNTER WITH A VORTEX WAKE. IF AN ONBOARD VORTEX ...

    SBIRPhase I1985Department of Transportation
  4. ROTARY WING HOVER PERFORMANCE PREDICTION

    Amount: $451,948.00

    THE ACCURATE PREDICTION OF THE PERFORMANCE OF A HELICOPTER ROTOR IN HOVER IS CRITICAL TO THE SUCCESS OF THE DESIGN. A NOVEL APPROACH TO THE SOLUTION OF THE HELICOPTER FREE WAKE HOVER PROBLEM IS ADDRES ...

    SBIRPhase II1984National Aeronautics and Space Administration
  5. TRANSIENT AND 3-D ROCKET ENGINE ANALYSIS

    Amount: $499,804.00

    THIS PROJECT ADDRESSES DEVELOPMENT OF ADVANCED COMPUTATIONALTECHNIQUES FOR ANALYSIS OF TRANSIENT AND THREE-DIMENSIONAL EFFECTS WITHIN ROCKET ENGINES. THE COMPUTATIONAL EFFICIENCYOF THESE NUMERICAL ANA ...

    SBIRPhase II1984National Aeronautics and Space Administration
  6. COMPUTER TECHNOLOGY TO EVALUATE AIRCRAFT VORTEX WAKE INTENSITY

    Amount: $49,573.00

    N/A

    SBIRPhase I1984Department of Transportation
  7. REDUCING U.S. IMPORT OIL DEPENDENCE BY ONE BILLION GALLONS OF DIESEL FUEL PER YEAR

    Amount: $39,000.00

    N/A

    SBIRPhase I1984National Science Foundation
  8. TRANSIENT AND 3-D ROCKET ENGINE ANALYSIS

    Amount: $49,000.00

    N/A

    SBIRPhase I1983National Aeronautics and Space Administration
  9. ROTARY WING HOVER PERFORMANCE PREDICTION

    Amount: $49,000.00

    N/A

    SBIRPhase I1983National Aeronautics and Space Administration
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