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Presentations

 

Contracts

Contract Information
(Sponsor, Title, SBIR/STTR Phase, Number, Award Date)

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NASA/Dryden, "Nonlinear Aerodynamics-Structure Time Simulation for HALE Aircraft Design/Analysis," STTR Phase I, NND05AA50C, January 2005



NASA/Dryden, "Model Updating Nonlinear System Identification Toolbox," SBIR Phase I, NND05AA44C, January 2005



USAF/AFRL/AFOSR, "Automated Design Optimization for Hypersonic Plasma-Aerodynamics," AFRL STTR Phase I, FA9550-04-C-0105, September 2004


NSF, "A Unified Coordinate Approach to a Gridless Computation," Phase I, DMI-0338537, January 2004



NASA/Glenn, "FILM-ID: Package for Identification of Multi-Dimensional Film Coefficient Maps," SBIR Phase I, NNC04CA42C, January 2004



NASA/LaRC, "Design Sensitivities of Response/Fatigue Life of Panels to Thermo-Acoustic Loads," SBIR Phase II, NNL04AA07C, December 2003



US Army/AMC, "Body-Flexure Control with Smart Actuation for Hypervelocity Missiles," SBIR Phase II, W31P4Q-04-C-R045, September 2003



USAF/AFRL, "Unified Gas-Kinetic Computational Algorithm for Continuum and Rarefied Flows," SBIR Phase I, F33615-03-M-3329, July 2003



NASA/DFRC, "Robust Aeroservoelastic Toolbox for Nonlinear Data-Based Modeling and Analysis," STTR Phase I, NAS4-03014, January 2003



NSF, "Highly Accurate Reconstruction Module for Multidisciplinary Computation," Phase I, DMI-0232255, January 2003



NASA/LaRC, "Design-Oriented Aeroservoelastic ZAERO Capability for 3D Configuration Shape MDO," SBIR Phase I, NAS1-03028, January 2003



NASA/LaRC ,"Design Sensitivities of Response/Fatigue Life of Panels to Thermo-Acoustic Loads," SBIR Phase I, NAS1-03021, January 2003



USAF/AFRL, "Integrated Hypersonic Aerothermoelastic Methodlogy for TAV/TPS Structural Design and Optimization," SBIR Phase II, F33615-02-C-3213, September 2002



USAF/AFRL, "Rapid Fatigue Life Projection for Thermal & Acoustic Loads," SBIR Phase I, F33615-02-M-3244, May 2002



USAF/46TW SKE/Eglin AFB, "An Integrated Rapid-Assessment of Flutter/Ejection Loads (RAFEL) Software System for Aircraft/Store Compatibility," SBIR Phase II, F08635-02-C-0107, June 2002



US Army/AMC, "Body-Flexure Control with Smart Actuation for Hypervelocity Missiles," SBIR Phase I, DAAH01-02-C-R098, January 2002



US Navy/Dahlgren, "Gun-Launched Projectile/Arizona Glider (AG) Design Concept as an ERGM and Reusable Launch Munition (RLM) Vehicle," SBIR Phase II, N00178-02-C-1007, November 2001



USAF/AFRL, "Fatigue Life of Composite Structures in Extreme Environments," SBIR Phase II, F33615-01-C-3111, June 2001



USAF/AFOSR, "NonLinear Reduced Order Modeling of Limit Cycle Oscillations of Aircraft Wings and Wing/Store," STTR Phase II, F49620-01-C-0029, May 2001



USAF/46TW SKE/Eglin AFB, "A Comprehensive Rapid-Assessment of Flutter/Ejection Loads (RAFEL) Software System for Aircraft/Store Compatibility," SBIR Phase I, F08635-01-C-0049, April 2001



USAF/AFRL, "Integrated Hypersonic Aerothermoelastic Methodlogy for TAV/TPS Structural Design and Optimization, SBIR Phase I, F33615-01-M-3131, March 2001



US Navy/Dahlgren, "Extended-Range Projectile Using Body-Conformal Oblique Wing/Tails with Smart Structure Control," SBIR Phase I, N00178-00-C-1051, May 2000



US Navy/NAWC, "Adaptive Reconfigurable Control Based on a Reduced Order System Identification for Flutter and Aeroservoelastic Instability Suppression," SBIR Phase I, N68335-00-C-0126, November 1999



US Navy/China Lake, "Optimized Fin Design Technologies for Improved Missile Control Authority, Maneuverability and Efficiency ," SBIR Phase II, N68936-99-C-0144, September 1999



USAF/AFOSR, "NonLinear Reduced Order Modeling of Limit Cycle Oscillations of Aircraft Wings," STTR Phase I, F49620-99-C-0050, August 1999



USAF/AFRL, "Formulation and Application of a Stochastic Fatigue Damage Accumulation Model for the Acoustic Response of Buckled Composite Panels," SBIR Phase I, F33615-99-C-3203, June 1999



USAF/AFRL, "Development of A Variable Stiffness Spar (VSS) Technology for Aircraft Maneuver Enhancement," SBIR Phase II, F33615-99-C-3202, May 1999


NASA/LaRC, "CFD/CSD Interfacing via an Innovative Structural Boundary Element Method," SBIR Phase II, NAS1-99076, March 1999



USAF/AFRL, "A Variable Stiffness Spar (VSS) Approach for Aircraft Maneuver Enhancement," SBIR Phase I, F33615-98-C-3204, April 1998


NASA/LaRC, "CFD/CSD Interfacing via an Innovative Structural Boundary Element Method," SBIR Phase I, NAS1-98051, April 1998



USAF/AFRL, "Development of the Aerodynamic/Aeroservoelastic Modules in ASTROS," STTR Phase II, F33615-96-C-3217, September 1996



USAF/AFRL, "Enhancement of the Aeroservoelastic Modules in ASTROS ," STTR Phase I, F33615-95-C-3219, September 1995



US Navy/China Lake, "Aeroelastic/ Aeroservoelastic Tailoring for Hinge Moment Minimization of Missile Fins," SBIR Phase I, N68936-97-C-0151, May 1995

 

Publications

 

ZONA51 (unsteady supersonic lifting surface aerodynamics)
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ZONA7 (unsteady supersonic wing-body aerodynamics)

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ZONA6 (unsteady subsonic wing-body aerodynamics)

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ZTAIC (unsteady transonic aerodynamics / transonic AIC method)

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ZTRAN (unsteady transonic aerodynamics using overset field panel method)

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ZONA7U (unsteady hypersonic/supersonic wing-body aerodynamics)

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g-Method for Flutter Solutions

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ASE (Aeroservoelasticity)

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ZSAP (Sonic Method)

  • Chen, P.C., and Liu, D.D., “Unsteady Sonic Aerodynamics Using Acceleration Potential Approach,” 44 th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Norfolk, VA, 7-10 April 2003, AIAA paper number 2003-1404.
  • Chen, P.C., and Liu, D.D., “Unsteady Wing-Body Aerodynamics for Aeroelastic Applications at Mach One,” International Forum on Aeroelasticity and Structural Dynamics 2003, Amsterdam, June 4-6, 2003.

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GLOADS (Gust Loads)

  • Karpel, M., Moulin, B., and Chen, P.C., “Dynamic Response of Aeroservoelastic Systems to Gust Excitations,” International Forum on Aeroelasticity and Structural Dynamics 2003, Amsterdam, June 4-6, 2003.

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NLFLTR (Nonlinear Flutter)

  • Chen, P.C., and Sulaeman, E., “Nonlinear Response of Aeroservoelastic Systems using Discrete State-Space Approach,” AIAA Journal, Vol. 41, No. 9, September 2003.

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ZAERO for MDO/Aeroservoelasticity/Smart Structure Control

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ZAERO for Limit Cycle Oscillation (LCO)

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ZAERO for Aeroelastic Tailoring Design/Optimization

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Other Selected Publications


Activities

In addition to commercial software development/licensing and private sector service contracts, ZONA Technology performs government research and development contracts. This page presents some of ZONA's current and past contracts, provides a publications list, and some presentations that are available for download. You can use the links below to jump to a section of interest.




 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

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