Amtec Engineering Inc

Company Information

Company Name
Amtec Engineering Inc
Address
P.o. Box 3633
Bellevue, WA, 00000
Phone
1 206-827-3304
URL
n/a
DUNS
n/a
Number of Employees
n/a

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,042,077.00
17
SBIR Phase II
$1,292,254.00
5
Chart code to be here

Award List

  1. THE DEVELOOPMENT OF A 3D VISCOUS FLOW ANALYSIS FOR THE EVALUATION OF HYERSONIC INLETS 4

    Amount: $233,553.00

    THE NEED EXISTS FOR AN EFFICIENT HYPERSONIC INLET FLOW ANALYSIS CODE THAT WILL CALCULATE BOTH EXTERNAL AND INTERNAL FLOW FIELDS INCLUDING VISCUS EFFECTS. THE FIRST OBJECTIVE OF THE PROPOSED EFFORT IS ...

    SBIR Phase II 1985 NavyDepartment of Defense
  2. FOR HIGH ENERGY LASER FLOWS

    Amount: $49,991.00

    AN EFFICIENT COMPUTATIONAL METHOD IS PROPOSED FOR MODELING THE COMPLEX PHYSICAL PHENOMENA OCCURING IN HIGH ENERGY CONTINUOUS WAVE LASER FLOW FIELDS. THESE FLOWS TYPICALLY CONTAIN BOUNDARY LAYERS, MIXI ...

    SBIR Phase I 1986 Air ForceDepartment of Defense
  3. THREE-DIMENSIONAL VISCOUS FLOW ANALYSIS FOR MOVING BODIES PAST FIXED STRUCTURES

    Amount: $50,000.00

    THE USE OF COMPUTER CODES THAT SIMULATE FLUID FLOWS IS BECOMING INCREASINGLY IMPORTANT IN THE DESIGN OF AIRCRAFT COMPONENTS. THE CURRENT STATE OF THE TECHNOLOGY OF NUMERICAL SIMULATION OF VISCOUS FLUI ...

    SBIR Phase I 1987 ArmyDepartment of Defense
  4. AN EFFICIENT 3D NAVIER-STOKES ANALYSIS FOR EVALUATION OF HYPERSONIC VEHICLES

    Amount: $161,000.00

    THE NEED EXISTS FOR A COST EFFECTIVE 3D FLOW ANALYSIS CODE THAT WILL ACCURATELY MODEL THE VISCOUS FLOW FIELDS FOR HYPERSONIC VEHICLES INCLUDING FLOW FEATURES THAT ARE ACTIVATED FOR THERMAL PROTECTION ...

    SBIR Phase II 1988 National Aeronautics and Space Administration
  5. ZONAL METHOD FOR MODELING POWERED-LIFT AIRCRAFT FLOW FIELDS

    Amount: $50,000.00

    ADVANCED SHORT TAKEOFF/VERTICAL LANDING AIRCRAFT ARE DESIGNED TO USE EXHAUST JETS TO DIRECTLY INCREASE LIFT. BEING ABLE TO NUMERICALLY MODEL THE FLOW FIELDS INVOLVED IN THESE DESIGNS WOULD GREATLY IMP ...

    SBIR Phase I 1988 National Aeronautics and Space Administration
  6. A 3D NAVIER-STOKES FLOW ANALYSIS FOR A LARGE-ARRAY MULTIPROCESSOR

    Amount: $50,000.00

    COMPUTATIONAL FLUID DYNAMICS (CFD) CODES HAVE BECOME IMPORTANT DESIGN AND ANALYSIS TOOLS FOR ENGINEERS, PARTICULARLY IN THE AEROSPACE INDUSTRY. CFD CODES, HOWEVER, ARE SEVERELY LIMITED BY THE COMPUTIN ...

    SBIR Phase I 1988 Defense Advanced Research Projects AgencyDepartment of Defense
  7. COUPLING GRID ADAPTION TO AN IMPLICIT NAVIER-STOKES SOLUTIONPROCEDURE

    Amount: $59,999.00

    A GRID ADAPTION PROCEDURE IS PROPOSED FOR A RECENTLY DEVELOPED CLASS OF NAVIER-STOKES SOLVERS WHICH USE RELAXATION RATHER THAN APPROXIMATE FACTORIZATION TO SOLVE THE LINEAR SYSTEM OF EQUATIONS. THE OB ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  8. HYPERSONIC ANALYSIS FOR VEHICLES IN THE CONTINUUM-TRANSITIONREGIME

    Amount: $49,925.00

    SEVERAL AEROSPACE VECHICLES ARE CURRENTLY BEING CONSIDERED THAT HAVE A SIGNIFICANT PORTION OF THEIR FLIGHT PATH IN THE UPPER REACHES OF THE ATMOSPHERE. THE FLOW ABOUT THESE VEHICLES IS IN THE CONTINUU ...

    SBIR Phase I 1991 National Aeronautics and Space Administration
  9. A ZONAL METHOD FOR MODELING POWERED-LIFT AIRCRAFT FLOW FIELDS

    Amount: $50,000.00

    ADVANCED SHORT TAKEOFF/VERTICAL LANDING AIRCRAFT ARE DESIGNED TO USE EXHAUST JETS DIRECTLY TO INCREASE LIFT. BEING ABLE TO MODEL NUMERICALLY THE FLOW FIELDS INVOLVED IN THESE DESIGNS WOULD GREATLY IMP ...

    SBIR Phase I 1991 National Aeronautics and Space Administration
  10. 30 POSTPROCESSING FOR COMPUTATIONAL FLUID DYNAMICS

    Amount: $50,000.00

    COMPUTATIONAL FLUID DYNAMICS (CFD) METHODS GENERATE VAST AMOUNTS OF NUMERICAL DATA THAT MUST BE DISPLAYED GRAPHICALLYFOR USE. CURRENT GRAPHICAL COMPUTER SOFTWARE PROGRAMS CAN DISPLAY DATA ONLY ON LINE ...

    SBIR Phase I 1991 National Aeronautics and Space Administration

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