A Comparative Analysis of the Response-Tracking Techniques in Aerospace Dynamic Systems Using Modal Participation Factors
Abstract
:1. Introduction
2. A Unified Concept
2.1. Modal Contribution
2.2. Modal Participation Factors
2.2.1. Class I: Static Modal Participation Factors (SMPFs)
The Steady-State Participation Factor
The Transient I Participation Factor: Maximum Modal Response
The Transient II Participation Factor: Time-Consistent Modal Response
Internal Load Participation Factor
2.2.2. Class II: Modal Relative Effectiveness Factors (MREFs)
Modal Effective Mass Participation Factor
Free–Free Modal Participation Factors
Modal Strain Energy Participation Factor
3. Sensitivity of Load via Static Modal Participation Factors
4. Proof of Concept
Approximate Derivative of Element Internal Load via SMPF
5. Case Study
Approximate Derivative of Element Internal Load via SMPF
6. Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Nomenclature
Matrices | |
Transformation matrix used to translate the internal forces to the element coordinate system | |
Matrix of transfer functions of the system | |
Stiffness matrix | |
Element stiffness matrix | |
Modal stiffness matrix | |
Mass matrix | |
Matrix of modal effective masses | |
Matrix of peak strain energies | |
Matrix of eigenvectors | |
Partition of the matrix of eigenvectors associated with the nodes of element e | |
Partition of the matrix of eigenvectors associated with the elastic modes | |
Partition of the matrix of eigenvectors associated with the rigid-body modes | |
Diagonal matrix of square natural frequencies | |
Diagonal matrix | |
Matrix of modal effective mass participation factors of size | |
Matrix equal to the product of | |
Vectors | |
Vector of enforced acceleration | |
Vector of dynamic responses for a unitary forcing function | |
Vector of peak dynamic responses for a unitary forcing function | |
External force vector | |
Time-dependent element internal load vector | |
Vector of time-dependent harmonic responses | |
Vector of nodal reaction forces | |
Vector of time-dependent nodal displacements | |
Vector of peak nodal displacements | |
Vector of time-dependent nodal acceleration | |
Eigenvector associated with the i-th mode | |
Scalars | |
Steady-state modal participation fraction | |
Transient modal participation fraction | |
Transient modal participation fraction II | |
Load participation fraction | |
Modal effective mass fraction | |
Modal strain energy participation fraction | |
Modal strain energy of the i-th mode at the j-th element | |
Total number of modes retained | |
Time-dependent strain energy | |
Subindex indicating a mode | |
Dynamic response of the i-th mode for a unitary forcing function. | |
Component of vector | |
Static response of the i-th mode to a unitary forcing function | |
Peak modal response of the i-th mode to a unitary forcing function | |
Response of the i-th mode to a unitary forcing function at the time instant | |
Nodal mass | |
Components of the matrix of modal effective masses | |
Modal mass of the i-th eigenvector | |
Number of nodes | |
Time domain function of the external force | |
Total number of rigid-body modes | |
Scalar function of the i-th harmonic mode Component of the harmonic response vector | |
r-th component of the load ( | |
Time | |
Time instant at which the peak response of the dominant mode occurs | |
Scalar time-dependent function of the displacement of the n-th nodeComponent of the vector of nodal displacements | |
Dynamic amplification factor of the i-th mode | |
Natural frequency of the i-th mode | |
Forcing frequency | |
Component of the eigenvector matrix located at row n, column i | |
Scalar time-dependent function of the modal contribution of the i-th mode atthe n-th node | |
Component of the matrix | |
Component of the diagonal matrix | |
Component of the modal effective mass participation factor matrix of size N × p | |
Free–free participation factor of the i-th mode | |
Trace of the elastic degrees of freedom |
References
- Martin, A.; Deierlein, G.G. Structural Topology Optimization of Tall Buildings for Dynamic Seismic Excitation Using Modal Decomposition. Eng. Struct. 2020, 216, 110717. [Google Scholar] [CrossRef]
- Kang, B.-S.; Park, G.-J.; Arora, J.S. A Review of Optimization of Structures Subjected to Transient Loads. Struct. Multidiscip. Optim. 2006, 31, 81–95. [Google Scholar] [CrossRef]
- Haug, E.J.; Arora, J.S. Applied Optimal Design: Mechanical and Structural Systems; John Wiley & Sons: Hoboken, NJ, USA, 1979; ISBN 047104170X. [Google Scholar]
- El Sayed, M.S.A.; Contreras, M.A.G.; Stathopoulos, N. Monitor Points Method for Loads Recovery in Static/Dynamic Aeroelasticity Analysis with Hybrid Airframe Representation. SAE Int. J. Aerosp. 2013, 6, 399. [Google Scholar] [CrossRef]
- Weng, S.; Xia, Y.; Xu, Y.-L.; Zhu, H.-P. An Iterative Substructuring Approach to the Calculation of Eigensolution and Eigensensitivity. J. Sound Vib. 2011, 330, 3368–3380. [Google Scholar] [CrossRef]
- Hsieh, C.C.; Arora, J.S. An Efficient Method for Dynamic Response Optimization. AIAA J. 1985, 23, 1454–1456. [Google Scholar] [CrossRef]
- Etman, L.F.P.; Van Campen, D.H.; Schoofs, A.J.G. Design Optimization of Multibody Systems by Sequential Approximation. Multibody Syst. Dyn. 1998, 2, 393–415. [Google Scholar] [CrossRef]
- Park, K.J.; Lee, J.N.; Park, G.J. Structural Shape Optimization Using Equivalent Static Loads Transformed from Dynamic Loads. Int. J. Numer. Methods Eng. 2005, 63, 589–602. [Google Scholar] [CrossRef]
- Kang, B.-S.; Park, G.J.; Arora, J.S. Optimization of Flexible Multibody Dynamic Systems Using the Equivalent Static Load Method. AIAA J. 2005, 43, 846–852. [Google Scholar] [CrossRef]
- Taghavi, S.; Miranda, E. Approximate Floor Acceleration Demands in Multistory Buildings. II: Applications. J. Struct. Eng. 2005, 131, 212–220. [Google Scholar] [CrossRef]
- Grandhi, R.V.; Haftka, R.T.; Watson, L.T. Design-Oriented Identification of Critical Times in Transient Response. AIAA J. 1986, 24, 649–656. [Google Scholar] [CrossRef]
- Grandhi, R.V.; Haftka, R.T.; Watson, L.T. Efficient Identification of Critical Stresses in Structures Subject to Dynamic Loads. Comput. Struct. 1986, 22, 373–386. [Google Scholar] [CrossRef]
- Choi, W.-S.; Park, G.-J. Structural Optimization Using Equivalent Static Loads at All Time Intervals. Comput. Methods Appl. Mech. Eng. 2002, 191, 2105–2122. [Google Scholar] [CrossRef]
- Arief, A.; Nappu, M.B.; Nizar, A.; Dong, Z.Y. Determination of DG Allocation with Modal Participation Factor to Enhance Voltage Stability. In Proceedings of the 8th International Conference on Advances in Power System Control, Operation and Management (APSCOM 2009), Hong Kong, China, 8–11 November 2009; IET: London, UK, 2009; pp. 1–6. [Google Scholar]
- Gebreselassie, A.; Chow, J.H. Investigation of the Effects of Load Models and Generator Voltage Regulators on Voltage Stability. Int. J. Electr. Power Energy Syst. 1994, 16, 83–89. [Google Scholar] [CrossRef]
- Arief, A.; Nappu, M.B.; Dong, Z.Y.; Arief, M. Under Voltage Load Shedding Incorporating Bus Participation Factor. In Proceedings of the 2010 Conference Proceedings IPEC, Singapore, 27–29 October 2010; IEEE: Piscataway, NJ, USA, 2010; pp. 561–566. [Google Scholar]
- Hashlamoun, W.A.; Hassouneh, M.A.; Abed, E.H. New Results on Modal Participation Factors: Revealing a Previously Unknown Dichotomy. IEEE Trans. Automat. Contr. 2009, 54, 1439–1449. [Google Scholar] [CrossRef]
- Tzounas, G.; Dassios, I.; Milano, F. Modal Participation Factors of Algebraic Variables. IEEE Trans. Power Syst. 2019, 35, 742–750. [Google Scholar] [CrossRef]
- Wallrapp, O.; Wiedemann, S. Simulation of Deployment of a Flexible Solar Array. Multibody Syst. Dyn. 2002, 7, 101–125. [Google Scholar] [CrossRef]
- Yun, C.-B.; Bahng, E.Y. Substructural Identification Using Neural Networks. Comput. Struct. 2000, 77, 41–52. [Google Scholar] [CrossRef]
- Zhou, Y.; Sun, Y.; Zeng, W. A Numerical Investigation on Stress Modal Analysis of Composite Laminated Thin Plates. Aerospace 2021, 8, 63. [Google Scholar] [CrossRef]
- Zhou, Y. Local Finite Element Refinement for Accurate Dynamic Stress via Modal Information Only. AIAA J. 2020, 58, 3593–3606. [Google Scholar] [CrossRef]
- Yang, Z.; Zhang, J.; Liu, K.; Zheng, Y.; Zhou, K.; Ma, S.; Wu, Z. Guided Wave Excitation and Sensing in Constant Irregular Cross Section Structures with the Semianalytical Finite-Element Method. J. Aerosp. Eng. 2022, 35, 4022020. [Google Scholar] [CrossRef]
- Asmussen, J.C. Modal Analysis Based on the Random Decrement Technique. Ph.D. Thesis, Department of Mechanical Engineering, Aalborg University, Aalborg, Denmark, 1997. [Google Scholar]
- Fang, S.M.; NIEDZWECKI, J.M. Comparison of Airfoil and Ribbon Fairings for Suppression of Flow-Induced Vibrations. Int. J. Comput. Methods Exp. Meas. 2014, 2, 30–45. [Google Scholar] [CrossRef]
- Van Langenhove, T.; Brughmans, M. Using MSC/NASTRAN and LMS/Pretest to Find an Optimal Sensor Placement for Modal Identification and Correlation of Aerospace Structures. Available online: https://www.researchgate.net/profile/M-Brughmans/publication/237114065_USING_MSCNASTRAN_AND_LMSPRETEST_TO_FIND_AN_OPTIMAL_SENSOR_PLACEMENT_FOR_MODAL_IDENTIFICATION_AND_CORRELATION_OF_AEROSPACE_STRUCTURES/links/568a4fa308ae1e63f1fbba4a/USING-MSC-NASTRAN-AND-LMS-PRETEST-TO-FIND-AN-OPTIMAL-SENSOR-PLACEMENT-FOR-MODAL-IDENTIFICATION-AND-CORRELATION-OF-AEROSPACE-STRUCTURES.pdf (accessed on 9 August 2023).
- Elghandour, E.; Kolkailah, F.A.; Mourad, A.H.I. Sensors Location Effect on the Dynamic Behaviour of the Composite Structure with Flaw Detection. In Proceedings of the 44th International SAMPE Symposium, Long Beach, CA, USA, 23 May 1999; Volume 44, pp. 349–358. [Google Scholar]
- Almitani, K.H.; Abdelrahman, A.A.; Eltaher, M.A. Influence of the Perforation Configuration on Dynamic Behaviors of Multilayered Beam Structure. Structures 2020, 28, 1413–1426. [Google Scholar] [CrossRef]
- Fouad, H.; Mourad, A.-H.I.; ALshammari, B.A.; Hassan, M.K.; Abdallah, M.Y.; Hashem, M. Fracture Toughness, Vibration Modal Analysis and Viscoelastic Behavior of Kevlar, Glass, and Carbon Fiber/Epoxy Composites for Dental-Post Applications. J. Mech. Behav. Biomed. Mater. 2020, 101, 103456. [Google Scholar] [CrossRef] [PubMed]
- MacNeal, R.H. The NASTRAN Theoretical Manual, (Level 15*5); HacNeal-Schwendler Corp.: Los Angeles, CA, USA, 1972. [Google Scholar]
- Irvine, T. Effective Modal Mass and Modal Participation Factors. 2013. Available online: http//www.Vib.com/tutorials2/ModalMass.pdf (accessed on 7 March 2007).
- Girard, A.; Roy, N.A. Modal Effective Parameters in Structural Dynamics. Rev. Eur. Des Éléments Finis 1997, 6, 233–254. [Google Scholar] [CrossRef]
- Kuhar, E.J.; Stahle, C.V. Dynamic Transformation Method for Modal Synthesis. AIAA J. 1974, 12, 672–678. [Google Scholar] [CrossRef]
- Lau, G.K.; Du, H. Topology Optimization of Head Suspension Assemblies Using Modal Participation Factor for Mode Tracking. Microsyst. Technol. 2005, 11, 1243–1251. [Google Scholar] [CrossRef]
- Photiadis, D.M.; Houston, B.H.; Liu, X.; Bucaro, J.A.; Marcus, M.H. Thermoelastic Loss Observed in a High Q Mechanical Oscillator. Phys. B Condens. Matter 2002, 316, 408–410. [Google Scholar] [CrossRef]
- Salmonte, A.J. Considerations on the Residual Contribution in Modal Analysis. Earthq. Eng. Struct. Dyn. 1982, 10, 295–304. [Google Scholar] [CrossRef]
- Carlbom, P.F. Combining MBS with FEM for Rail Vehicle Dynamics Analysis. Multibody Syst. Dyn. 2001, 6, 291–300. [Google Scholar] [CrossRef]
- Wilson, E.L.; Yuan, M.; Dickens, J.M. Dynamic Analysis by Direct Superposition of Ritz Vectors. Earthq. Eng. Struct. Dyn. 1982, 10, 813–821. [Google Scholar] [CrossRef]
- Chen, J.-T.; Hong, H.; Yeh, C.-S. Modal Reaction Method for Modal Participation Factors in Support Motion Problems. Commun. Numer. Methods Eng. 1995, 11, 479–490. [Google Scholar] [CrossRef]
- Chen, J.-T.; Chen, K.H.; Chen, I.L.; Liu, L.W. A New Concept of Modal Participation Factor for Numerical Instability in the Dual BEM for Exterior Acoustics. Mech. Res. Commun. 2003, 30, 161–174. [Google Scholar] [CrossRef]
- Hamzi, B.; Abed, E.H. Local Modal Participation Analysis of Nonlinear Systems Using Poincaré Linearization. Nonlinear Dyn. 2020, 99, 803–811. [Google Scholar] [CrossRef]
- Oh, B.K.; Kim, M.S.; Kim, Y.; Cho, T.; Park, H.S. Model Updating Technique Based on Modal Participation Factors for Beam Structures. Comput. Civ. Infrastruct. Eng. 2015, 30, 733–747. [Google Scholar] [CrossRef]
- Chopra, A.K.; Chintanapakdee, C. Drift Spectrum vs. Modal Analysis of Structural Response to near-Fault Ground Motions. Earthq. Spectra 2001, 17, 221–234. [Google Scholar] [CrossRef]
- Palermo, M.; Silvestri, S.; Gasparini, G.; Trombetti, T. Seismic Modal Contribution Factors. Bull. Earthq. Eng. 2015, 13, 2867–2891. [Google Scholar] [CrossRef]
- Ghahari, S.F.; Abazarsa, F.; Ghannad, M.A.; Taciroglu, E. Response-only Modal Identification of Structures Using Strong Motion Data. Earthq. Eng. Struct. Dyn. 2013, 42, 1221–1242. [Google Scholar] [CrossRef]
- Igusa, T.; Der Kiureghian, A.; Sackman, J.L. Modal Decomposition Method for Stationary Response of Non-classically Damped Systems. Earthq. Eng. Struct. Dyn. 1984, 12, 121–136. [Google Scholar] [CrossRef]
- Whittaker, A.S.; Constantinou, M.C.; Ramirez, O.M.; Johnson, M.W.; Chrysostomou, C.Z. Equivalent Lateral Force and Modal Analysis Procedures of the 2000 NEHRP Provisions for Buildings with Damping Systems. Earthq. Spectra 2003, 19, 959–980. [Google Scholar] [CrossRef]
- Miranda, E.; Taghavi, S. Approximate Floor Acceleration Demands in Multistory Buildings. I: Formulation. J. Struct. Eng. 2005, 131, 203–211. [Google Scholar] [CrossRef]
- Wilson, E.L.; Der Kiureghian, A.; Bayo, E.P. A Replacement for the SRSS Method in Seismic Analysis. Earthq. Eng. Struct. Dyn. 1981, 9, 187–192. [Google Scholar] [CrossRef]
- Romera, L.; Hernandez, S. An Improved Technique for Modal Contribution Factors of Dynamic Responses. In Proceedings of the 40th Structures, Structural Dynamics, and Materials Conference and Exhibit, St. Louis, MO, USA, 12–15 April 1999; p. 1242. [Google Scholar]
- Przekop, A.; Rizzi, S.A.; Groen, D.S. Nonlinear Acoustic Response of an Aircraft Fuselage Sidewall Structure by a Reduced-Order Analysis. In Proceedings of the Ninth International Conference on Recent Advances in Structural Dynamics, Southampton, UK, 17–19 July 2006. [Google Scholar]
- Zhang, L.; Brincker, R.; Andersen, P. Modal Indicators for Operational Modal Identification. In Proceedings of the IMAC 19: A Conference on Structural Dynamics, Kissimmee, FL, USA, 5–8 February 2001; Society for Experimental Mechanics: Bethel, CT, USA, 2001; pp. 746–752. [Google Scholar]
- Chopra, A.K. Dynamics of Structures: Theory and Applications to Earthquake Engineering; Civil Engineering and Engineering Mechanics Series; Prentice Hall: Hoboken, NJ, USA, 2012; ISBN 9780132858038. [Google Scholar]
- Chopra, A.K. Modal Analysis of Linear Dynamic Systems: Physical Interpretation. J. Struct. Eng. 1996, 122, 517–527. [Google Scholar] [CrossRef]
- Wijker, J.J. Spacecraft Structures; Springer Science & Business Media: Berlin/Heidelberg, Germany, 2008; ISBN 3540755535. [Google Scholar]
- Hizarci, B.; Kıral, Z.; Şahin, S. Optimal Extended State Observer Based Control for Vibration Reduction on a Flexible Cantilever Beam with Using Air Thrust Actuator. Appl. Acoust. 2022, 197, 108944. [Google Scholar] [CrossRef]
- Darabseh, T.T.; Tarabulsi, A.M.; Mourad, A.-H.I. Active Flutter Suppression of a Two-Dimensional Wing Using Linear Quadratic Gaussian Optimal Control. Int. J. Struct. Stab. Dyn. 2022, 22, 2250157. [Google Scholar] [CrossRef]
- Zghal, S.; Frikha, A.; Dammak, F. Static Analysis of Functionally Graded Carbon Nanotube-Reinforced Plate and Shell Structures. Compos. Struct. 2017, 176, 1107–1123. [Google Scholar] [CrossRef]
- Frikha, A.; Zghal, S.; Dammak, F. Dynamic Analysis of Functionally Graded Carbon Nanotubes-Reinforced Plate and Shell Structures Using a Double Directors Finite Shell Element. Aerosp. Sci. Technol. 2018, 78, 438–451. [Google Scholar] [CrossRef]
- Zghal, S.; Frikha, A.; Dammak, F. Non-Linear Bending Analysis of Nanocomposites Reinforced by Graphene-Nanotubes with Finite Shell Element and Membrane Enhancement. Eng. Struct. 2018, 158, 95–109. [Google Scholar] [CrossRef]
- Frikha, A.; Zghal, S.; Dammak, F. Finite Rotation Three and Four Nodes Shell Elements for Functionally Graded Carbon Nanotubes-Reinforced Thin Composite Shells Analysis. Comput. Methods Appl. Mech. Eng. 2018, 329, 289–311. [Google Scholar] [CrossRef]
- Zghal, S.; Frikha, A.; Dammak, F. Large Deflection Response-Based Geometrical Nonlinearity of Nanocomposite Structures Reinforced with Carbon Nanotubes. Appl. Math. Mech. 2020, 41, 1227–1250. [Google Scholar] [CrossRef]
- Kim, J.; Lee, P. An Enhanced Craig–Bampton Method. Int. J. Numer. Methods Eng. 2015, 103, 79–93. [Google Scholar] [CrossRef]
- Kammer, D.C.; Cessna, J.; Kostuch, A. An Effective Mass Measure for Selecting Free-Free Target Modes. In Proceedings of the 23rd International Modal Analysis Conference, Orlando, FL, USA, 31 January–3 February 2005. [Google Scholar]
- Li, H.; Yang, H.; Hu, S.-L.J. Modal Strain Energy Decomposition Method for Damage Localization in 3D Frame Structures. J. Eng. Mech. 2006, 132, 941–951. [Google Scholar] [CrossRef]
- Li, L.; Hu, Y.; Wang, X. Numerical Methods for Evaluating the Sensitivity of Element Modal Strain Energy. Finite Elem. Anal. Des. 2013, 64, 13–23. [Google Scholar] [CrossRef]
- Lim, T.W. Structural Damage Detection Using Modal Test Data. AIAA J. 1991, 29, 2271–2274. [Google Scholar] [CrossRef]
- Haftka, R.T.; Adelman, H.M. Recent Developments in Structural Sensitivity Analysis. Struct. Optim. 1989, 1, 137–151. [Google Scholar] [CrossRef]
- Babu, S.S.; Mourad, A.-H.I.; Al-Nuaimi, S. Numerical Assessment of Interlaminar Stresses in Tapered Composite Laminates: A Comparative Analysis with FEM and VAM. In Proceedings of the 2022 Advances in Science and Engineering Technology International Conferences (ASET), Dubai, United Arab Emirates, 21–24 February 2022; pp. 1–6. [Google Scholar]
- Suresh Babu, S.; Mourad, A.-H.I. Assessment of Interlaminar Stress Components in Laminated Composites Manufactured by Ply-Drop Technique. In Proceedings of the ASME 2021 International Mechanical Engineering Congress and Exposition, Online, 1–5 November 2021. [Google Scholar]
- Zghal, S.; Frikha, A.; Dammak, F. Mechanical Buckling Analysis of Functionally Graded Power-Based and Carbon Nanotubes-Reinforced Composite Plates and Curved Panels. Compos. Part B Eng. 2018, 150, 165–183. [Google Scholar] [CrossRef]
- Zghal, S.; Trabelsi, S.; Dammak, F. Post-Buckling Behavior of Functionally Graded and Carbon-Nanotubes Based Structures with Different Mechanical Loadings. Mech. Based Des. Struct. Mach. 2022, 50, 2997–3039. [Google Scholar] [CrossRef]
- Trabelsi, S.; Frikha, A.; Zghal, S.; Dammak, F. Thermal Post-Buckling Analysis of Functionally Graded Material Structures Using a Modified FSDT. Int. J. Mech. Sci. 2018, 144, 74–89. [Google Scholar] [CrossRef]
- Shampine, L.F.; Reichelt, M.W. The Matlab Ode Suite. SIAM J. Sci. Comput. 1997, 18, 1–22. [Google Scholar] [CrossRef]
- Bertsekas, D. Nonlinear Programming; Athena Scientific Optimization and Computation Series; Athena Scientific: Nashua, NH, USA, 2016; ISBN 9781886529052. [Google Scholar]
- Thomas, P.V.; ElSayed, M.S.A.; Walch, D. Development of High Fidelity Reduced Order Hybrid Stick Model for Aircraft Dynamic Aeroelasticity Analysis. Aerosp. Sci. Technol. 2019, 87, 404–416. [Google Scholar] [CrossRef]
- Zhang, C.; Zhang, S.; Santo, H.; Cai, M.; Yu, M.; Si, M. Combining Reduced-Order Stick Model with Full-Order Finite Element Model for Efficient Analysis of Self-Elevating Units. J. Mar. Sci. Eng. 2023, 11, 119. [Google Scholar] [CrossRef]
- Zghal, S.; Frikha, A.; Dammak, F. Free Vibration Analysis of Carbon Nanotube-Reinforced Functionally Graded Composite Shell Structures. Appl. Math. Model. 2018, 53, 132–155. [Google Scholar] [CrossRef]
- Zghal, S.; Trabelsi, S.; Frikha, A.; Dammak, F. Thermal Free Vibration Analysis of Functionally Graded Plates and Panels with an Improved Finite Shell Element. J. Therm. Stress. 2021, 44, 315–341. [Google Scholar] [CrossRef]
- Hoblit, F.M. Gust Loads on Aircraft: Concepts and Applications; AIAA: Washington, DC, USA, 1988. [Google Scholar]
Mode | (12) | (14) | (16) | (22) | (25) |
---|---|---|---|---|---|
1 | 0.8558 | 0.8627 | 0.8658 | 0.8819 | 0.1993 |
2 | 0.0934 | 0.0890 | 0.0872 | 0.0851 | 0.1996 |
3 | 0.0318 | 0.0302 | 0.0294 | 0.0225 | 0.2029 |
4 | 0.0136 | 0.0129 | 0.0126 | 0.0088 | 0.1987 |
5 | 0.0054 | 0.0051 | 0.0050 | 0.0016 | 0.1995 |
Element | Actual Peak Load (N) | (N) | % Error | (N) | % Error | (N) | % Error |
---|---|---|---|---|---|---|---|
1 | 53.1225 | 48.9718 | −7.8134% | 57.9858 | 9.1550% | 53.0976 | −0.0467% |
2 | 53.7885 | 49.9985 | −7.0461% | 45.8251 | −14.8049% | 53.8574 | 0.1282% |
3 | 51.5479 | 48.6080 | −5.7032% | 49.1496 | −4.6525% | 51.5973 | 0.0959% |
4 | 51.3453 | 49.3883 | −3.8114% | 65.4091 | 27.3906% | 51.3164 | −0.0563% |
5 | 51.2290 | 50.5989 | −1.2300% | 38.6055 | −24.6413% | 51.0221 | −0.4039% |
It | Element 1 | Element 2 | Element 3 | Element 4 | Element 5 | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Finite Diff | Error | Finite Diff | Error | Finite Diff | Error | Finite Diff | Error | Finite Diff | Error | ||||||
1 | −1.730 | −1.730 | 0.000 | −2.820 | −2.820 | 0.000 | −1.627 | −1.627 | 0.000 | −2.662 | −2.662 | 0.000 | −1.646 | −1.646 | 0.000 |
2 | −1.616 | −1.730 | 0.114 | −2.880 | −2.820 | −0.060 | −1.692 | −1.627 | −0.065 | −2.685 | −2.662 | −0.022 | −1.888 | −1.646 | −0.242 |
3 | −1.853 | −1.734 | −0.119 | −2.645 | −2.846 | 0.201 | −1.683 | −1.627 | −0.056 | −2.566 | −2.684 | 0.118 | −1.889 | −1.644 | −0.245 |
4 | −1.873 | −1.734 | −0.139 | −3.116 | −2.869 | −0.247 | −1.630 | −1.624 | −0.006 | −2.963 | −2.703 | −0.260 | −1.894 | −1.641 | −0.253 |
5 | −1.403 | −1.731 | 0.328 | −2.763 | −2.891 | 0.128 | −1.332 | −1.619 | 0.287 | −2.806 | −2.721 | −0.086 | −1.944 | −1.636 | −0.308 |
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Nieto, M.G.; Babu, S.S.; ElSayed, M.S.A.; Mourad, A.-H.I. A Comparative Analysis of the Response-Tracking Techniques in Aerospace Dynamic Systems Using Modal Participation Factors. Appl. Mech. 2023, 4, 1038-1065. https://0-doi-org.brum.beds.ac.uk/10.3390/applmech4040053
Nieto MG, Babu SS, ElSayed MSA, Mourad A-HI. A Comparative Analysis of the Response-Tracking Techniques in Aerospace Dynamic Systems Using Modal Participation Factors. Applied Mechanics. 2023; 4(4):1038-1065. https://0-doi-org.brum.beds.ac.uk/10.3390/applmech4040053
Chicago/Turabian StyleNieto, Michelle Guzman, Sandeep Suresh Babu, Mostafa S. A. ElSayed, and Abdel-Hamid Ismail Mourad. 2023. "A Comparative Analysis of the Response-Tracking Techniques in Aerospace Dynamic Systems Using Modal Participation Factors" Applied Mechanics 4, no. 4: 1038-1065. https://0-doi-org.brum.beds.ac.uk/10.3390/applmech4040053