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NIELSEN ENGINEERING & RESEARCH, INC.
UEI: N/A
# of Employees: 4
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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DRAG REDUCTION ON AN EJECTION SEAT DURING HIGH SPEED EJECTION
Amount: $59,283.00N/A
SBIRPhase I1990Department of Defense Navy -
SUPERSONIC TURBULENT REACTING FLOW MODELING AND CALCULATION
Amount: $384,697.00THE MODELING AND CALCULATION OF SUPERSONIC TURBULENT REACTING FLOWS ARE CONSIDERED. IT IS SUGGESTED THAT ACCURATE PREDICTION OF SUCH FLOW FIELDS DEPENDS ON A THERMOCHEMICAL MODEL THAT, WHILE BEING SIM ...
SBIRPhase II1989National Aeronautics and Space Administration -
ANALYSIS OF LOW FLYING MISSILES VERSUS VARIOUS SEA STATES
Amount: $529,256.00A PROGRAM OF WORK IS PROPOSED LEADING TO THE PREDICTION AND UNDERSTANDING OF THE AERODYNAMICS ACTING ON A MISSILE OR AN AIRPLANE FLYING AT LOW ALTITUDE OVER THE SEA SURFACE. IT APPEARS THAT CLOSE TO T ...
SBIRPhase II1989Department of Defense Navy -
PREDICTION OF TORPEDO GUIDANCE WIRE POSTLAUNCH INTERFERENCE WITH MANEUVERING SUBMARINES
Amount: $57,900.00A PROGRAM OF WORK LEADING TO AN ANALYTICAL CAPABILITY TO PREDICT THE POSTLAUNCH BEHAVIOR OF TORPEDO GUIDANCE WIRES IN THE VICINITY OF MANEUVERING SUBMARINES IS DESCRIBED. AN EXISTING METHOD TO PREDICT ...
SBIRPhase I1989Department of Defense Navy -
UNSTRUCTURED TRIANGULAR MESH/NAVIER-STOKES METHOD FOR AERODYNAMICS OF AIRCRAFT WITH ICE ACCRETION
Amount: $50,000.00N/A
SBIRPhase I1989National Aeronautics and Space Administration -
PREDICTION METHOD FOR ASTOVL GROUND EFFECTS FLOWS
Amount: $265,000.00NUMERICAL PREDICTIONS OF GROUND EFFECTS FLOW SUFFER LOSS OF ACCURACY BECAUSE OF INADEQUATE TURBULENCE MODELS AND BECAUSE OF THE INABILITY TO TREAT COMPLEX AIRCRAFT GEOMETRY IN AN ECONOMICAL MANNER. ON ...
SBIRPhase II1988Department of Defense Defense Advanced Research Projects Agency -
EXPLOITATION OF MULTIPLE SOLUTIONS OF THE NAVIER-STOKES EQUATIONS TO ACHIEVE RADICALLY IMPROVED FLIGHT
Amount: $58,021.00IT IS KNOWN THAT THE NONLINEAR NAVIER-STOKES EQUATIONS WILL MODEL MOST FLUID FLOW OF AERONAUTICAL INTEREST. THE EXISTENCE AND UNIQUENESS OF THE SOLUTION TO THE NAVIER-STOKES EQUATIONS HAVE NOT BEEN PR ...
SBIRPhase I1988Department of Defense Air Force -
A COMPUTATIONAL MODEL FOR THRUST REVERSING AND VECTORED JETS
Amount: $55,225.00N/A
SBIRPhase I1988Department of Defense Air Force -
ANALYSIS OF LOW FLYING MISSILES VERSUS VARIOUS SEA STATES
Amount: $59,588.00N/A
SBIRPhase I1988Department of Defense Navy -
SUPERSONIC TURBULENT REACTING FLOW MODELING AND CALCULATION
Amount: $49,979.00N/A
SBIRPhase I1988National Aeronautics and Space Administration
