CONTINUUM DYNAMICS INC

Company Information

Company Name
CONTINUUM DYNAMICS INC
Address
34 LEXINGTON AVE
TRENTON, NJ, 08618-2302
Phone
1 609-538-0444
URL
http://www.continuum-dynamics.com
DUNS
096857313
Number of Employees
23
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$10,194,082.23
130
SBIR Phase II
$34,834,937.00
61
STTR Phase I
$269,894.00
3
STTR Phase II
$1,298,768.00
2
Chart code to be here

Award List

  1. Flight Adaptive Blade for Optimum Rotor Response (FABFORR)

    Amount: $99,987.00

    While past research has demonstrated the utility and benefits to be gained with the application of advanced rotor system control concepts, none have been implemented to date on a production military o ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  2. Advanced Methods for Predicting 3D Unsteady Flows Around Wind Turbines

    Amount: $99,990.00

    Wind power has an important role in satisfying the power needs of the United States. Since wind power is a clean renewable source of energy, it also serves an important role in reducing dependence on ...

    STTR Phase I 2010 Department of Energy
  3. Advanced Electrostatic Computation in Molecular Dynamics

    Amount: $738,861.00

    DESCRIPTION (provided by applicant): Advances in computational hardware and molecular modeling techniques have revolutionized our ability to simulate electrostatic interactions, which play a fundament ...

    SBIR Phase II 2010 Department of Health and Human Services
  4. Fast Lifting Surface Models for Rotorcraft Analysis

    Amount: $69,862.00

    Current comprehensive rotorcraft analyses typically use lifting line theories coupled with 2D look-up tables to determine rotor blade lift, drag and pitching moment. These methods cannot directly capt ...

    SBIR Phase I 2010 ArmyDepartment of Defense
  5. Active Flight Control and Applique Inceptor Concepts for Autorotation Performance Enhancement

    Amount: $79,990.00

    Enhancing rotorcraft safety due to engine or drive train failures has been a primary concern throughout the history of vertical flight operations. Recent work on autorotation trajectory optimization h ...

    SBIR Phase I 2010 NavyDepartment of Defense
  6. Measurement and Modeling of the Debye Effect in Hydroacoustics

    Amount: $79,929.00

    Since submarines operate in an ionic seawater environment, there exists the possibility that any of several recognized electro-kinetic mechanisms may be excited and produce potentially detectable elec ...

    SBIR Phase I 2010 NavyDepartment of Defense
  7. 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 ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  8. 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 ...

    SBIR Phase II 1984 National Aeronautics and Space Administration
  9. 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 ...

    SBIR Phase II 1985 Department of Transportation
  10. 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 ...

    SBIR Phase I 1985 Department of Transportation

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