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ZONA TECHNOLOGY INC
UEI: LYMKH9UK64J7
# of Employees: 7
HUBZone Owned: No
Socially and Economically Disadvantaged: Yes
Woman Owned: No
Award Charts
Award Listing
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FUN3D-based Adjoint Optimization for Elastic Tandem Airfoils in Chaotic Flows
Amount: $149,999.00This proposal develops a two-dimensional, FUN3D-based, flow-structure-coupled adjoint optimization framework capable of handling chaotic dynamics, and validate this framework on an elastic tandem airf ...
STTRPhase I2017Department of Defense Air Force -
Dynamic Flight Simulation Utilizing High Fidelity CFD-Based Nonlinear Reduced Order Model
Amount: $124,929.00The 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 -
Uniformed Aeroelastic ROM Realization Across Flight Parameter Space for Dynamic Flight Simulation
Amount: $149,949.00ABSTRACT: The proposed effort will focus on the development of the parameterized Navier-Stokes (NS) based ROM for the Dynamic Flight Simulation (DFS) framework. The F/A-18 Active Aeroelastic Wing (AAW ...
SBIRPhase I2016Department of Defense Air Force -
RANS-Based Stick-to-Stress Dynamic Flight Simulation for Aircraft Life Prediction
Amount: $149,978.00ABSTRACT: Both commercial and military aircraft are being flown/utilized for extended operational time. The aircraft cumulative flight hours often extends the original design limits. Each aircraft man ...
SBIRPhase I2016Department of Defense Air Force -
Development of an Efficient Flutter and Limit Cycle Oscillation Predictive Tool
Amount: $748,611.00In this Phase II effort, an accurate, user-friendly, well validated, and production-ready efficient flutter and Limit Cycle Oscillation (LCO) predictive tool will be developed. The ZONA Euler Unsteady ...
STTRPhase II2016Department of Defense Air Force -
Linearized FUN3D for Rapid Aeroelastic and Aeroservoelastic Design and Analysis
Amount: $749,959.00In 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 -
Development of an Efficient Flutter and Limit Cycle Oscillation Predictive Tool
Amount: $149,906.00ABSTRACT: 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 Air Force -
Stick-to-Stress Dynamic Flight Simulation for Predicting Fatigue Life and Scheduling Inspections of Aircraft
Amount: $749,789.00ABSTRACT: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 Air Force -
Stick-to-Stress Dynamic Flight Simulation for Predicting Fatigue Life and Scheduling Inspections of Aircraft
Amount: $149,939.00ABSTRACT: 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 I2014Department of Defense Air Force -
Real-Time Mode Shape and Aeroelastic System Identification Toolset for Flight Test
Amount: $747,125.00ABSTRACT: 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 Air Force