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Sukra Helitek Inc.
UEI: NG59DUUYTJT5
# of Employees: 3
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: Yes
Award Charts
Award Listing
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A Computational Tool for High Advance Ratio Configurations
Amount: $124,682.00Newer vertical lift configurations consider speed as an important design parameter with forward speeds upwards of 230 Knots, which is well above the acceptable incompressible flow regime. In such high ...
SBIRPhase I2014National Aeronautics and Space Administration -
RotCFD: A Viscous Design Tool for Advanced Configurations
Amount: $749,394.00During initial design studies, parametric variation of vehicle geometry is routine. In addition, rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Correlation be ...
SBIRPhase II2012National Aeronautics and Space Administration -
An Aero-Acoustic Tool for Terminal Area Operations
Amount: $124,991.00In this highly interconnected world, transportation systems must feature increased flexibility and shorter door-to-door trip times to be successful. Shorter door-to-door trip times require an increas ...
SBIRPhase I2012National Aeronautics and Space Administration -
RotCFD: A Viscous Design Tool for Advanced Configurations
Amount: $99,781.00The incorporation of viscous analysis in design is vital for a completeunderstanding of aerodynamic problems.This proposal offers to develop and integrate with RotCFD a method for semi-automatically g ...
SBIRPhase I2011National Aeronautics and Space Administration -
Computational Wind Tunnel: A Design Tool for Rotorcraft
Amount: $598,888.00During initial design studies, parametric variation of vehicle geometry is routine. In addition, rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Estimation of ...
SBIRPhase II2009National Aeronautics and Space Administration -
Computational Wind Tunnel: A Design Tool for Rotorcraft
Amount: $99,527.00Rotorcraft engineers traditionally use the wind tunnel to evaluate and finalize designs. Insufficient correlation between wind tunnel results and flight tests, have been often attributed in part to u ...
SBIRPhase I2008National Aeronautics and Space Administration -
Rapid Computational Fluid Dynamics (CFD) Methodology for Rotorcraft Maneuver Analysis
Amount: $729,776.00The lack of proper estimation of air loads encountered during transient maneuvers introduces excessive design conservatism. A reduced fidelity CFD methodology based on momentum source (Rot3DC) and a c ...
SBIRPhase II2008Department of Defense Army -
Rapid Computational Fluid Dynamics (CFD) Methodology for Rotorcraft Maneuver Analysis
Amount: $118,644.00The lack of proper estimation of air loads encountered during transient maneuvers introduces excessive design conservatism. This proposal offers to develop a computational tool, based on the lower or ...
SBIRPhase I2006Department of Defense Army -
Automated Generation of Viscous CFD Grids for Increased Productivity of High Fidelity Aerodynamic Analysis
Amount: $727,154.00Viscous analysis is vital for a complete understanding of missile and UAV aerodynamic properties. A high fidelity aerodynamic analysis tool capable of predicting a flow field can significantly reduce ...
SBIRPhase II2004Department of Defense Army -
A Preliminary Design Tool for Shrouded-Fans
Amount: $728,344.00Shrouded-fans play a key role in the U.S. Army's transportation systems. A preliminary design tool capable of simulating the flow field in different flight conditions for predicting the shroud and fan ...
SBIRPhase II2003Department of Defense Army
