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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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Generation of CFD-Based Structurally Independent Aerodynamic Influence Coefficient Matrix
Amount: $749,728.00The primary technical objective of Phase II is to develop ZONArsquo;s next-generation commercial software for aeroelastic, aeroservoelastic, and dynamic loads analysis using the CFD-based AIC matrices ...
SBIRPhase II2021National Aeronautics and Space Administration -
Generation of CFD-Based Structurally Independent Aerodynamic Influence Coefficient Matrix
Amount: $124,904.00Despite advances in Computational Fluid Dynamics (CFD) methods; application of CFD to an aeroelastic analysis is still not well-accepted by the aerospace industry. Currently, the unsteady panel method ...
SBIRPhase I2020National Aeronautics and Space Administration -
Bayesian-Based Probabilistic Limit Cycle Oscillation Prediction of Aircraft with Stores
Amount: $749,989.00The overall technical objective of the Phase II effort is to extend the Phase I developments and achieve a fully predictive Bayesian-based, data driven, probabilistic prediction tool of the F-16 limit ...
STTRPhase II2020Department of Defense Air Force -
Discrete Time State-Space Aeroservoelastic Modeling using FUN3D
Amount: $749,974.00The overall technical objective of the Phase II effort is to make OVERFUN as a fully multi-functional aeroelastic software system that can establish either the discrete time state-space plant model or ...
SBIRPhase II2019National Aeronautics and Space Administration -
Bayesian-Based Probabilistic Limit Cycle Oscillation Prediction of Aircraft with Stores
Amount: $149,921.00The overall technical objective of the Phase I effort is to develop a Bayesian-based, data driven, probabilistic limit cycle oscillation (LCO) prediction tool that can be used to identify critical and ...
STTRPhase I2019Department of Defense Air Force -
FUN3D-based Sensitivity Analysis for F-15 in Chaotic Flows
Amount: $749,918.00The overall technical objective of the Phase II effort is to develop a FUN3D-based adjoint framework using the Non-Intrusive Least Squares Shadowing (NI-LSS) for sensitivity analysis of complex config ...
STTRPhase II2019Department of Defense Air Force -
Discrete Time State-Space Aeroservoelastic Modeling using FUN3D
Amount: $124,176.00CFD-based reduced order modeling (ROM) has been an active research area, as they can be used directly with common linear flutter analysis tools. Among them, linearized reduced-order modeling approache ...
SBIRPhase I2018National Aeronautics and Space Administration -
Uniformed Aeroelastic ROM Realization Across Flight Parameter Space for Dynamic Flight Simulation
Amount: $747,340.00The technical objective of the Phase II project is to develop the production-ready Dynamic Flight Simulation (DFS) system using the F-15 Saudi as a testbed and validate it with the F-15 Saudi flight t ...
SBIRPhase II2018Department of Defense Air Force -
Dynamic Flight Simulation Utilizing High Fidelity CFD-Based Nonlinear Reduced Order Model
Amount: $734,526.00The Nonlinear Dynamic Flight Simulation (NL-DFS) system will be developed in the Phase II project by combining the classical nonlinear rigid-body flight dynamics model with an add-on nonlinear aeroela ...
SBIRPhase II2017National Aeronautics and Space Administration -
Multiple Level Reduced Order Modeling for Ship Airwake Modeling and Simulation
Amount: $124,818.00The overall technical objective of the Phase I effort is to develop a Multi-Level Reduced Order Model (ML-ROM) for the airwake flow field to reduce the storage requirements by a factor of 1000 or more ...
STTRPhase I2017Department of Defense Navy