Sukra Helitek Inc.

Address

IA
Ames, IA, 50014-4504

Information

DUNS: 877929125
# of Employees: 3

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: Y

Award Charts




Award Listing

  1. A Computational Tool for High Advance Ratio Configurations

    Amount: $124,682.00

    Newer 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
  2. RotCFD: A Viscous Design Tool for Advanced Configurations

    Amount: $749,394.00

    During 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
  3. An Aero-Acoustic Tool for Terminal Area Operations

    Amount: $124,991.00

    In 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
  4. RotCFD: A Viscous Design Tool for Advanced Configurations

    Amount: $99,781.00

    The 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
  5. Computational Wind Tunnel: A Design Tool for Rotorcraft

    Amount: $598,888.00

    During 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
  6. Computational Wind Tunnel: A Design Tool for Rotorcraft

    Amount: $99,527.00

    Rotorcraft 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
  7. Rapid Computational Fluid Dynamics (CFD) Methodology for Rotorcraft Maneuver Analysis

    Amount: $729,776.00

    The 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 II2008Army Department of Defense
  8. Rapid Computational Fluid Dynamics (CFD) Methodology for Rotorcraft Maneuver Analysis

    Amount: $118,644.00

    The 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 I2006Army Department of Defense
  9. Automated Generation of Viscous CFD Grids for Increased Productivity of High Fidelity Aerodynamic Analysis

    Amount: $727,154.00

    Viscous 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 II2004Army Department of Defense
  10. A Preliminary Design Tool for Shrouded-Fans

    Amount: $728,344.00

    Shrouded-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 II2003Army Department of Defense

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