ZONA TECHNOLOGY, INC

Address

9489 EIRONWOOD SQ DR STE 100
SCOTTSDALE, AZ, 85258-4578

http://www.zonatech.com

Information

DUNS: 182103291
# of Employees: 10

Ownership Information

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

Award Charts




Award Listing

  1. Dynamic Flight Simulation Utilizing High Fidelity CFD-Based Nonlinear Reduced Order Model

    Amount: $124,929.00

    The overall technical objective of the Phase I effort is to develop a nonlinear aeroelastic solver utilizing the FUN3D generated nonlinear aerodynamic Reduced Order Model (ROM). Two types of aerodyna ...

    SBIRPhase I2016National Aeronautics and Space Administration
  2. Linearized FUN3D for Rapid Aeroelastic and Aeroservoelastic Design and Analysis

    Amount: $749,959.00

    In Phase I, a prototypical FUN3D-based ZONA Euler Unsteady Solver (FunZEUS) was developed to generate the Generalized Aerodynamic Forces (GAFs) due to structural modes, control surface kinematic modes ...

    SBIRPhase II2015National Aeronautics and Space Administration
  3. Development of an Efficient Flutter and Limit Cycle Oscillation Predictive Tool

    Amount: $149,906.00

    ABSTRACT: Several current fighter aircraft with external store configurations persistently encounter Limit Cycle Oscillation (LCO) problems. A fast and accurate aeroelastic prediction is required to ...

    STTRPhase I2015Department of Defense
  4. Stick-to-Stress Dynamic Flight Simulation for Predicting Fatigue Life and Scheduling Inspections of Aircraft

    Amount: $749,789.00

    ABSTRACT:Both commercial and military aircraft are being flown/utilized for extended operational time; a more accurate prediction of residual life and the inspection interval for an individual aircraf ...

    SBIRPhase II2015Department of Defense
  5. Stick-to-Stress Dynamic Flight Simulation for Predicting Fatigue Life and Scheduling Inspections of Aircraft

    Amount: $149,939.00

    ABSTRACT: Both commercial and military aircraft are being flown/utilized for extended operational time. The aircraft cumulative flight hours often times extends the original design limits. Each diffe ...

    SBIRPhase I2014Air Force Department of Defense
  6. Real-Time Mode Shape and Aeroelastic System Identification Toolset for Flight Test

    Amount: $747,125.00

    ABSTRACT: The ability to extract structure mode shapes, accurate system frequency/damping and to predict the onset of flutter/LCO in a real-time capacity from flight/wind tunnel test data are some of ...

    SBIRPhase II2014Department of Defense
  7. Sensitivity Analysis Methods for Complex, Multidisciplinary Systems

    Amount: $746,893.00

    ABSTRACT: The overall technical objective of this Phase II effort is to develop computational tools for computing response sensitivities of parametric multi-disciplinary air vehicle systems that exhi ...

    STTRPhase II2014Department of Defense
  8. CFD-Based Over-Determined Trim Analysis for Optimum Aerodynamic Efficiency

    Amount: $124,538.00

    The overall objective of this Phase I project is to develop a nonlinear trim module in FUN3D for enabling the determined and over-determined trim analyses to be performed by FUN3D with static aeroelas ...

    SBIRPhase I2014National Aeronautics and Space Administration
  9. Linearized FUN3D for Rapid Aeroelastic and Aeroservoelastic Design and Analysis

    Amount: $124,813.00

    The overall objective of this Phase I project is to develop a hybrid approach in FUN3D, referred herein to as the Linearized FUN3D, for rapid aeroelastic and aeroservoelastic (ASE) design and analysis ...

    SBIRPhase I2014National Aeronautics and Space Administration
  10. Innovative Structural and Material Concepts for Low-Weight Low-Drag Aircraft Design

    Amount: $749,997.00

    The overall technical objective of this multi-phase project is to develop and validate a so-called 'AAW-Process' that consists of (i) the Active Aeroelastic Wing (AAW) technology of employing multiple ...

    SBIRPhase II2014National Aeronautics and Space Administration

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