Complere, Inc.

Company Information

Company Name
Complere, Inc.
Address
P.O. Box 541
Pacific Grove, CA, 93950 0541
Phone
1 831-646-5370
URL
n/a
DUNS
64773401
Number of Employees
5
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$679,561.00
12
SBIR Phase II
$2,087,719.00
4

Award List

  1. CURRENTLY, THE RATE OF DEVELOPMENT OF COMPUTATIONAL FLUID DYNAMICS IS NO LONGER DEPENDENT ON COMPUTER SIZE OR NUMERICAL TECHNIQUES.

    Amount: $45,000.00

    CURRENTLY, THE RATE OF DEVELOPMENT OF COMPUTATIONAL FLUID DYNAMICS IS NO LONGER DEPENDENT ON COMPUTER SIZE OR NUMERICAL TECHNIQUES. FURTHER PROGRESS IS RESTRICTED BY THE NEED FOR RELIABLE TEST CASES A ...

    SBIR Phase I 1983 National Aeronautics and Space Administration
  2. MEASUREMENT OF VORTEX FLOWFIELDS

    Amount: $500,000.00

    MANY SUPERSONIC AIRCRAFT GENERATE VORTICES AT HIGHLY-SWEPT LEADING EDGES WHICH GENERALLY AUGMENT THE LIFT. HOWEVER, OUR CURRENT UNDERSTANDING OF VORTEX, VISCOUS/INVISCID INTERACTIONS IS INSUFFICIENT T ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  3. AN ASSESSMENT OF LASER VELOCIMETER POTENTIAL IN HYPERSONIC FLOWS

    Amount: $494,000.00

    AT PRESENT, PROGRESS IN COMPUTATIONAL FLUID DYNAMICS OF HIGHSPEED FLOWS IS RESTRICTED BY THE NEED FOR EXPERIMENTAL DATA WHICH CAN BE USED FOR THE DEVELOPMENT OF EMPIRICAL TURBULENCE MODELS AND TO VALI ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  4. TURBULENT SHEAR STRESS MEASUREMENTS IN HYPERSONIC FLOW

    Amount: $49,510.00

    ALTHOUGH EXTENSIVE PROGRESS HAS BEEN MADE IN COMPUTATIONAL FLUID MECHANICS, RELIABLE FLIGHT VEHICLE DESIGNS AND MODIFICATIONS STILL CANNOT BE MADE WITHOUT RECOURSE TO EXTENSIVE WIND TUNNEL TESTING. FU ...

    SBIR Phase I 1987 Air ForceDepartment of Defense
  5. A LASER BASED TRANSITION DETECTOR

    Amount: $49,389.00

    ONE OF THE LARGEST SOURCES OF UNCERTAINTY IN PROPOSED HYPERSONIC TESTING OF THE NATIONAL AEROSPACE PLANE WILL BE THE MEASUREMENT OF THE EXTENT OF LAMINAR FLOW ON WIND TUNNELTEST MODELS WITH FREE AND F ...

    SBIR Phase I 1988 National Aeronautics and Space Administration
  6. AN OPTICAL ANGLE OF ATTACK SENSOR

    Amount: $495,550.00

    A MAJOR SOURCE OF TRANSONIC AND SUPERSONIC WIND TUNNEL TEST DATA UNCERTAINTY IS DUE TO ANGLE OF ATTACK MEASUREMENT ERRORCAUSED BY UNKNOWN STING AND BALANCE DEFLECTIONS UNDER LOAD. SINCE DYNAMIC LOADS ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  7. Laser Fluorescence Anemometer for Oceanographic Instrumentation

    Amount: $48,241.00

    Efficient and cost effective ocean outfall dilution systems are essential to the health of the ocean enviroment. Unfortunately, wasterfield transport and subsequent ocean outfall dilution are complex ...

    SBIR Phase I 1993 NavyDepartment of Defense
  8. Measurement of Fuel Spray Interactions

    Amount: $77,570.00

    Quantitative measurement of spray patterns is of fundamental importance in the development of efficient and practical aerospace propulsion and power systems. At present, there is considerable interes ...

    SBIR Phase I 1996 Office of the Secretary of DefenseDepartment of Defense
  9. Hypersonic Free-Flight Measurement of Aeroshell Forces and Flowfields

    Amount: $69,871.00

    A Hypersonic Gun Tunnel and laser based high speed imaging systems will be used to generate a unique, free flight, aerodynamic data base of potential Mars aeroshell configurations. These experiments ...

    SBIR Phase I 2006 National Aeronautics and Space Administration
  10. AN OPTICAL ANGLE OF ATTACK SENSOR

    Amount: $47,000.00

    N/A

    SBIR Phase I 1988 National Aeronautics and Space Administration

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