HR job title
- Senior Professor
- Contact Info
- 1 979 845 1694
Strganac, Thomas Professor
Positions
- Professor, Aerospace Engineering, College of Engineering
Research Areas
- Overview
- Publications
- Teaching
- Works By Students
- Background
- Contact
- Other
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Overview
Publications
selected publications
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academic article
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Patterson, R., Scholten, W., Strganac, T., Turner, T., & Hartl, D.
(2020).
Experimental validation of a shape-memory alloy slat-cove filler: Structural response and computational model development. Journal of Intelligent Material Systems and Structures.
31(17), 1986-2001.
-
Yang, Y. i., & Strganac, T. W.
(2013).
Experiments of Vortex-Induced Torsional Oscillation of a Flat Plate in Cross Flow. AIAA Journal.
51(6), 1522-1526.
-
Prime, Z., Cazzolato, B., Doolan, C., & Strganac, T.
(2010).
Linear-Parameter-Varying Control of an Improved Three-Degree-of-Freedom Aeroelastic Model. Journal of Guidance, Control, and Dynamics.
33(2), 615-619.
-
Lee, Y. S., Kerschen, G., McFarland, D. M., Hill, W. J., Nichkawde, C., Strganac, T. W., Bergman, L. A., & Vakakis, A. F.
(2007).
Suppressing aeroelastic instability using broadband passive targeted energy transfers, part 2: Experiments. AIAA Journal.
45(10), 2391-2400.
-
Strganac, T. W.
(2007).
Physics-Based Aeroelastic Analysis for Future Air Vehicle Concepts Using a Fully Nonlinear Methodology
-
Platanitis, G., & Strganac, T. W.
(2005).
Suppression of control reversal using leading- and trailing-edge control surfaces. Journal of Guidance, Control, and Dynamics.
28(3), 452-460.
-
Thompson, D. E., & Strganac, T. W.
(2005).
Nonlinear analysis of store-induced limit cycle oscillations. Nonlinear Dynamics.
39(1-2), 159-178.
-
Clark, R., Cox, D., Curtiss, H. C., Edwards, J. W., Hall, K. C., Peters, D. A., ... Strganac, T. W.
(2004).
A Modern Course in Aeroelasticity. Solid Mechanics and Its Applications.
116, 1-766.
-
Beran, P. S., Strganac, T. W., Kim, K., & Nichkawde, C
(2004).
Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities. Nonlinear Dynamics.
37(4), 323-339.
-
Platanitis, G., & Strganac, T. W.
(2004).
Control of a nonlinear wing section using leading- and trailing-edge surfaces. Journal of Guidance, Control, and Dynamics.
27(1), 52-58.
-
Kurdila, A. J., Li, J., Strganac, T., & Webb, G.
(2003).
Nonlinear control methodologies for hysteresis in PZT actuated on-blade elevons. Journal of Aerospace Engineering.
16(4), 167-176.
-
Dowell, E., Edwards, J., & Strganac, T.
(2003).
Nonlinear Aeroelasticity. Journal of Aircraft.
40(5), 857-874.
-
Strganac, T. W.
(2003).
Book Reviews. AIAA Journal.
41(4), 752-753.
-
Gilliatt, H. C., Strganac, T. W., & Kurdila, A. J.
(2003).
An investigation of internal resonance in aeroelastic systems. Nonlinear Dynamics.
31(1), 1-22.
-
Ko, J., Strganac, T. W., Junkins, J. L., Akella, M. R., & Kurdila, A. J.
(2002).
Structured model reference adaptive control for a wing section with structural nonlinearity. Journal of Vibration and Control.
8(5), 553-573.
-
Sheta, E. F., Harrand, V. J., Thompson, D. E., & Strganac, T. W.
(2002).
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems. Journal of Aircraft.
39(1), 133-141.
-
Kurdila, A. J., Prazenica, R. J., Rediniotis, O., & Strganac, T.
(2001).
Multiresolution Methods for Reduced-Order Models for Dynamical Systems. Journal of Guidance, Control, and Dynamics.
24(2), 193-200.
-
Kurdila, A. J., Strganac, T. W., Junkins, J. L., Ko, J., & Akella, M. R.
(2001).
Nonlinear Control Methods for High-Energy Limit-Cycle Oscillations. Journal of Guidance, Control, and Dynamics.
24(1), 185-192.
-
Strganac, T. W., Ko, J., Thompson, D. E., & Kurdila, A. J.
(2000).
Identification and control of limit cycle oscillations in aeroelastic systems. Journal of Guidance, Control, and Dynamics.
23(6), 1127-1133.
-
Golden, H. J., Strganac, T. W., & Schapery, R. A.
(1999).
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses. Journal of Applied Mechanics, Transactions ASME.
66(4), 872-878.
-
Ko, J. H., Strganac, T. W., & Kurdila, A. J.
(1999).
Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity. Nonlinear Dynamics.
18(3), 289-301.
-
Block, J. J., & Strganac, T. W.
(1998).
Applied active control for a nonlinear aeroelastic structure. Journal of Guidance, Control, and Dynamics.
21(6), 838-845.
-
Ko, J. W., Strganac, T. W., & Kurdila, A. J.
(1998).
Stability and control of a structurally nonlinear aeroelastic system. Journal of Guidance, Control, and Dynamics.
21(5), 718-725.
-
O’Neil, T., & Strganac, T. W.
(1998).
Aeroelastic response of a rigid wing supported by nonlinear springs. Journal of Aircraft.
35(4), 616-622.
-
Ko, J., Kurdila, A. J., & Strganac, T. W.
(1997).
Adaptive Feedback Linearization for the Control of a Typical Wing Section With Structural Nonlinearity. ASME -Publications- Ad.
53, 139-148.
-
Ko, J., Kurdila, A. J., & Strganac, T. W.
(1997).
Nonlinear control of a prototypical wing section with torsional nonlinearity. Journal of Guidance, Control, and Dynamics.
20(6), 1181-1189.
-
Golden, H. J., Strganac, T. W., & Schapery, R. A
(1996).
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses. ASME -Publications- Ad.
51, 91-100.
-
Strganac, T. W., & Golden, H. J.
(1996).
Predictions of nonlinear viscoelastic behavior using a hybrid approach. International Journal of Solids and Structures.
33(30), 4561-4570.
-
Strganac, T. W., & Kim, Y. I.
(1996).
Aeroelastic behavior of composite plates subject to damage growth. Journal of Aircraft.
33(1), 68-73.
-
STRGANAC, T. W., & IKKIM, Y.
(1995).
THE EFFECT OF DAMAGE GROWTH ON THE AEROELASTIC RESPONSE OF COMPOSITE STRUCTURES. Mechanics of Advanced Materials and Structures.
2(4), 329-342.
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STRGANAC, T. W., LETTON, A., PAYNE, D. F., & BISKUP, B. A.
(1995).
CHARACTERIZATION OF NONLINEAR VISCOELASTIC BEHAVIOR USING A DYNAMIC-MECHANICAL APPROACH. AIAA Journal.
33(5), 904-910.
-
STRGANAC, T. W., LETTON, A., ROCK, N. I., WILLIAMS, K. D., & FARROW, D. A.
(1995).
CHARACTERIZATION OF POLYMER-FILMS RETRIEVED FROM NASA LONG-DURATION EXPOSURE FACILITY. Journal of Spacecraft and Rockets.
32(3), 502-506.
-
Kurdila, A. J., Menon, R., & Strganac, T. W.
(1993).
Constraint violation in concurrent range space methods for transient dynamic analysis. Computing Systems in Engineering.
4(4-6), 435-444.
-
STRGANAC, T. W., & MOOK, D. T.
(1990).
NUMERICAL-MODEL OF UNSTEADY SUBSONIC AEROELASTIC BEHAVIOR. AIAA Journal.
28(5), 903-909.
-
Patterson, R., Scholten, W., Strganac, T., Turner, T., & Hartl, D.
(2020).
Experimental validation of a shape-memory alloy slat-cove filler: Structural response and computational model development. Journal of Intelligent Material Systems and Structures.
31(17), 1986-2001.
-
chapter
-
Dowell, E., Bendiksen, O., Edwards, J., & Strganac, T.
(2010).
Transonic Nonlinear Aeroelasticity. Encyclopedia of Aerospace Engineering.
Wiley.
-
Fabiano, R. H., Kurdila, A. J., & Strganac, T.
(1993).
Robust Control of Distributed Parameter Systems with Structured Uncertainty. Computation and Control III.
(pp. 193-201).
Springer Nature.
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Dowell, E., Bendiksen, O., Edwards, J., & Strganac, T.
(2010).
Transonic Nonlinear Aeroelasticity. Encyclopedia of Aerospace Engineering.
Wiley.
-
conference paper
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Leaton, A., Scholten, W., Lieb, K., Hartl, D. J., Strganac, T., & Turner, T. L.
(2020).
Aerostructural and Aeroacoustic Experimental Testing of Shape Memory Alloy Slat Cove Filler
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Scholten, W., Patterson, R., Eustice, M., Cook, S., Hartl, D., Strganac, T., & Turner, T.
(2018).
AERODYNAMIC AND STRUCTURAL EVALUATION OF AN SMA SLAT-COVE FILLER USING COMPUTATIONAL AND EXPERIMENTAL TOOLS AT MODEL SCALE. v001t04a019-v001t04a019.
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Scholten, W. D., Patterson, R., Chapelon, Q., Hartl, D. J., Strganac, T. W., & Turner, T. L.
(2017).
Experimentation and Computational Assessment of an SMA-Based Slat-Cove Filler For Noise Reduction in a High Lift Wing
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Oremland, J., Suryakumar, V. S., Strganac, T. W., & Mangalam, A. S.
(2017).
Flutter Suppression of an Aeroelastic Wing Using Aerodynamic Observables, Leading-Edge, and Trailing-Edge Control Surfaces
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Scholten, W. D., Patterson, R. D., Hartl, D. J., Strganac, T. W., Chapelon, Q., & Turner, T. L.
(2017).
Computational and experimental fluid-structure interaction assessment of a high-lift wing with a slat-cove filler for noise reduction
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Suryakumar, V. S., Babbar, Y., Strganac, T. W., & Mangalam, A. S.
(2016).
Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point. Journal of Aircraft.
1626-1637.
-
Suryakumar, V. S., Mangalam, A. S., Babbar, Y., & Strganac, T. W.
(2016).
A Load-Based Feedback Approach for Distributed Aeroservoelastic Control
-
Scholten, W., Patterson, R., Hartl, D., Strganac, T., Volpi, J., Chapelon, Q., & Turner, T.
(2016).
NOISE REDUCTION IN A HIGH LIFT WING USING SMAS: COMPUTATIONAL FLUID-STRUCTURAL ANALYSIS. v001t02a009-v001t02a009.
-
Scholten, W., Hartl, D., Strganac, T., & Turner, T.
(2016).
REDUCTION OF ACTUATION LOADS IN A SELF-DEPLOYING SMA-BASED SLAT-COVE FILLER FOR A TRANSPORT AIRCRAFT. v002t04a016-v002t04a016.
-
Suryakumar, V. S., Babbar, Y., Strganac, T. W., & Mangalam, A. S.
(2015).
An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point
-
Suryakumar, V. S., Babbar, Y., Strganac, T. W., & Mangalam, A. S.
(2015).
Control of a Nonlinear Wing Section using Fly-by-Feel Sensing
-
Babbar, Y., Suryakumar, V. S., Strganac, T. W., & Mangalam, A. S.
(2015).
Measurement and Modeling of Aeroelastic Response under Gust
-
Babbar, Y., Suryakumar, V. S., Mangalam, A., & Strganac, T. W.
(2013).
An approach for prescribed experiments for aerodynamic-structural dynamic interaction
-
Babbar, Y., Suryakumar, V. S., & Strganac, T. W.
(2013).
Experiments in free and forced aeroelastic response
-
Suryakumar, V. S., & Strganac, T. W.
(2013).
A Finite element-Multibody dynamics co-simulation methodology applied to FAST. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
-
Suryakumar, V. S., & Strganac, T. W.
(2013).
A Finite element-Multibody dynamics co-simulation methodology applied to FAST
-
Babbar, Y., Suryakumar, V. S., & Strganac, T. W.
(2013).
Experiments in Aeroelastic Response and Control under Gust. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
-
Babbar, Y., Suryakumar, V. S., & Strganac, T. W.
(2013).
Experiments in Aeroelastic Response and Control under Gust
-
Yang, Y., & Strganac, T. W.
(2012).
Experiments of vortex-induced vibration of a flat plate exposed to a normal cross flow
-
Yang, Y. i., & Strganac, T.
(2012).
Experiments of Vortex-Induced Vibration of a Flat Plate Exposed to a Normal Cross Flow. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
-
Niksch, A., Valasek, J., Strganac, T., & Carlson, L.
(2009).
Six Degree-of-Freedom Dynamical Model of a Morphing Aircraft
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Lucas, A., Valasek, J., & Strganac, T.
(2009).
Gust Load Alleviation of an Aeroelastic System Using Nonlinear Control. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
-
Jackson, J., Bhattacharya, R., & Strganac, T.
(2008).
Modelling and Suboptimal Trajectory Generation for a Symmetric Flapping Wing Vehicle
-
Niksch, A., Valasek, J., Carlson, L., & Strganac, T.
(2008).
Morphing Aircaft Dynamical Model: Longitudinal Shape Changes
-
Hill, W. J., Strganac, T. W., Nichkawde, C., McFarland, D. M., Kerschen, G., Lee, Y. S., Vakakis, A. F., & Bergman, L. A.
(2006).
Suppression of aeroelastic instability with a nonlinear energy sink: Experimental results. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
3145-3157.
-
Nichkawde, C., Strganac, T., & Beran, P.
(2006).
Nonlinear Aeroelastic Response of the Flexible Wing in Trim. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
436-455.
-
Hill, W., Strganac, T., Nichkawde, C., McFarland, D., Kerschen, G., Lee, Y., Vakakis, A., & Bergman, L.
(2006).
Suppression of Limit Cycle Oscillations with a Nonlinear Energy Sink: Experimental Results
-
Silva, W., Strganac, T., & Hajj, M.
(2005).
Higher-Order Spectral Analysis of a Nonlinear Pitch and Plunge Apparatus. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
2643-2662.
-
Beran, P., Hur, J., Snyder, R., Strong, D., Bryson, D., & Strganac, T.
(2005).
Static Nonlinear Aeroelastic Analysis of a Blended Wing Body
-
Beran, P. S., Strganac, T. W., Kim, K., & Nichkawde, C.
(2004).
Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities. Nonlinear Dynamics.
323-339.
-
Kim, K., & Strganac, T.
(2004).
The Effects of External Stores on Nonlinear Aeroelastic Responses. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
4525-4548.
-
Dowell, E. H., Edwards, J., & Strganac, T.
(2003).
Nonlinear Aeroelasticity. Journal of Aircraft.
-
Platanitis, G., & Strganac, T. W
(2003).
Analyses and experiments of suppression of control reversal using a wing section with multiple control surfaces. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
776-787.
-
Kim, K. U., & Strganac, T. W.
(2003).
Nonlinear responses of a cantilever wing with an external store. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
2781-2795.
-
Platanitis, G., & Strganac, T.
(2003).
Analyses and Experiments of Suppression of Control Reversal Using a Wing Section with Multiple Control Surfaces
-
Dowell, E., Edwards, J., & Strganac, T.
(2003).
Nonlinear Aeroelasticity. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
3824-3847.
-
Kim, K., & Strganac, T.
(2003).
Nonlinear Responses of a Cantilever Wing with an External Store
-
Beran, P., Strganac, T., & Kim, K.
(2003).
Studies of Store-Induced Limit Cycle Oscillations Using a Model with Full System Nonlinearities. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
3026-3039.
-
Kim, K., & Strganac, T.
(2002).
Aeroelastic Studies of a Cantilever Wing with Structural and Aerodynamic Nonlinearities
-
Platanitis, G., & Strganac, T.
(2002).
Control of a Wing Section With Structural Nonlinearities Using Leading and Trailing Edge Control Surfaces
-
Sheta, E. F., Harrand, V. J., Thompson, D. E., & Strganac, T. W.
(2002).
Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems. Journal of Aircraft.
133-141.
-
Rao, P., Strganac, T., & Rediniotis, O.
(2000).
Control of aeroelastic response via synthetic jet actuators
-
Thompson, D., & Strganac, T.
(2000).
Store-induced limit cycle oscillations and internal resonances in aeroelastic systems
-
Sheta, E., Harrand, V., Thompson, D., & Strganac, T.
(2000).
Computational and experimental investigation of limit cycle oscillations in nonlinear aeroelastic systems
-
Rao, P., Gilarranz, J., Ko, J., Strganac, T., & Rediniotis, O.
(2000).
Flow separation control via synthetic jet actuation
-
Strganac, T., Ko, J., Thompson, D., & Kurdila, A.
(1999).
Identification and control of limit cycle oscillations in aeroelastic systems
-
Kurdila, A., Prazenica, C., Rediniotis, O., & Strganac, T.
(1999).
Multiresolution methods for reduced order models for dynamical systems
-
Kurdila, A., Rediniotis, O., Strganac, T., & Ko, J.
(1999).
Multiwavelets and Particle Image Velocimetry methods
-
Strganac, T., Junkins, J., Ko, J., & Kurdila, A. J.
(1999).
Nonlinear Control Methods for High Energy Limit Cycle Oscillations. 3215-3226.
-
Ko, J., Akella, M. R., Junkins, J. L., Strganac, T. W., & Kurdila, A. J.
(1999).
Nonlinear Model Reference Adaptive Control for Limit Cycle Oscillations. 3203-3213.
-
Ko, J., Strganac, T., & Kurdila, A.
(1998).
Nonlinear adaptive control of an aeroelastic system via geometric methods
-
Gilliatt, H., Strganac, T., & Kurdila, A.
(1998).
On the presence of internal resonances in aeroelastic systems
-
Gadhok, J., Belur, R., Strganac, T. W., & Junkins, J. L.
(1997).
A laser scanning graphic system for multimedia podium presentations. Proceedings of SPIE.
191-201.
-
Golden, H., Strganac, T., Schapery, R., Golden, H., Strganac, T., & Schapery, R.
(1997).
An approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses
-
Gilliatt, H., Strganac, T., Kurdila, A., Gilliatt, H., Strganac, T., & Kurdila, A.
(1997).
Nonlinear aeroelastic response of an airfoil
-
Ko, J., Kurdila, A., Strganac, T., Ko, J., Kurdila, A., & Strganac, T.
(1997).
Nonlinear control theory for a class of structural nonlinearities in a prototypical wing section
-
Golden, H. J., Strganac, T. W., & Schapery, R. A
(1996).
Approach to characterize nonlinear viscoelastic material behavior using dynamic mechanical tests and analyses. 225.
-
O'Neil, T., Gilliatt, H., & Strganac, T.
(1996).
Investigations of aeroelastic response for a system with continuous structural nonlinearities
-
Golden, H., Strganac, T., & Schapery, R.
(1996).
A test and analysis protocol to rapidly characterize nonlinear viscoelastic properties of balloon materials
-
Rand, J., Grant, D., & Strganac, T.
(1996).
The nonlinear biaxial characterization of balloon film
-
O'Neil, T., & Strganac, T.
(1995).
Nonlinear aeroelastic response - Analyses and experiments
-
Strganac, T., Kurdila, A., Kim, C., & Kim, Y.
(1994).
Dynamic response and game theoretic control of evolving structural systems
-
Payne, D., Biskup, B., Letton, A., & Strganac, T.
(1994).
Viscoelastic characterization of thin-film materials using a dynamic mechanical approach
-
KO, J., KURDILA, A., PARK, S., & STRGANAC, T.
(1993).
Calculation of Numerical Boundary Measure for Wavelet-Galerkin Approximations in Aeroelasticity
-
PAYNE, D., BISKUP, B., LETTON, A., & STRGANAC, T.
(1993).
ON NONLINEAR VISCOELASTIC ANALYSIS OF THIN FILM MATERIALS USING A DYNAMIC MECHANICAL APPROACH
-
STRGANAC, T., LETTON, A., & FARROW, A.
(1993).
PHYSICAL CHARACTERIZATION OF THIN-FILM POLYMERS EXPOSED TO THE LOW EARTH ORBIT ENVIRONMENT
-
KO, J., KIM, C., KURDILA, A., & STRGANAC, T.
(1993).
Wavelet Galerkin METHODES FOR GAME THEORETIC CONTROL OF DISTRIBUTED PARAMETER SYSTEMS
-
STRGANAC, T., FARROW, D., LETTON, A., WILLIAMS, K., & ROCK, N.
(1992).
Analysis and simulation of polymers exposed to low earth orbit (LEO)environments
-
STRGANAC, T., & LETTON, A.
(1991).
The investigation of balloon materials exposed to the low earth orbit environment
-
WHITLOW, W., BENNETT, R. M., & STRGANAC, T. W.
(1989).
ANALYSIS OF VIBRATIONS OF THE NATIONAL TRANSONIC FACILITY MODEL SUPPORT SYSTEM USING A 3-D AEROELASTIC CODE. 398-407.
-
STRGANAC, T.
(1988).
A study of aeroelastic stability for the model support system of theNational Transonic Facility
-
STRGANAC, T., & MOOK, D.
(1987).
A new method to predict unsteady aeroelastic behavior
-
STRGANAC, T., MITCHUM, M., & MOOK, D.
(1987).
The numerical simulation of subsonic flutter
-
STRGANAC, T., & MOOK, D.
(1986).
Application of the unsteady vortex-lattice method to the nonlinear two-degree-of-freedom aeroelastic equations
-
Leaton, A., Scholten, W., Lieb, K., Hartl, D. J., Strganac, T., & Turner, T. L.
(2020).
Aerostructural and Aeroacoustic Experimental Testing of Shape Memory Alloy Slat Cove Filler
Teaching
teaching activities
- AERO201 Intro To Flight Instructor
- AERO289 Sptp: Intro To Flight Mechanic Instructor
- AERO301 Theoretical Aerodyn Instructor
- AERO420 Aeroelasticity Instructor
- AERO481 Hnr-seminar Instructor
- AERO491 Hnr-research Instructor
- AERO491 Hnr-research Instructor
- AERO689 Sptp: Structural Dynamics Aer Instructor
- AERO689 Sptp:aeroelast And Strct Dynm Instructor
- AERO691 Research Instructor
Works By Students
chaired theses and dissertations
-
Babbar, Yogesh (2015-05). Aeroelastic Response of a Typical Wing Section under Nonlinearities and Gust Loads.
-
Jackson, Justin Patrick (2008-08). Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.
-
Johnson, Kristen Holmstrom (2010-08). Reduced-sensing Control Methods for Infinite-dimensional Systems.
-
Kim, Kiun (2004-09). Nonlinear aeroelastic analysis of aircraft wing-with-store configurations.
-
Kutz, Douglas M (2014-05). An Updated Procedure for Tare and Interference Wind Tunnel Testing of Strut-Mounted Models.
-
Lucas, Amy Marie (2009-08). Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control.
-
Nichkawde, Chetan (2003-05). Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation.
-
Scholten, William David (2016-12). Analysis and Wind Tunnel Testing of a Superelastic Slat-Cove Filler for Airframe Noise Reduction.
-
Suryakumar, Vishvas Samuel (2013-05). A Finite Element-Multibody Dynamics Co-simulation Methodology Applied to FAST.
-
Suryakumar, Vishvas Samuel (2016-12). Fly-by-Feel Aeroservoelasticity.
-
Yang, Yi (2010-12). Experimental Investigations of Vortex Induced Vibration of A Flat Plate in Pitch Oscillation.
Background
education and training
Contact
first name
- Thomas
has last name
- Strganac
mailing address
-
Texas A&M University
Aerospace Engineering
3141 TAMU
College Station, TX 77843-3141
USA
Other
- strag@tamu.edu