Relevant bibliographies by topics / Wings (Anatomy) – Structural dynamics

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Wings (Anatomy) – Structural dynamics'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Wings (Anatomy) – Structural dynamics"

1

Santini, P., and P. Gasbarri. "Structural Dynamics of Composite Wings." Journal of Reinforced Plastics and Composites 17, no. 4 (1998): 319–60. http://dx.doi.org/10.1177/073168449801700403.

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2

Liu, Long, Hongda Li, Haisong Ang, and Tianhang Xiao. "Numerical investigation of flexible flapping wings using computational fluid dynamics/computational structural dynamics method." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 1 (2016): 85–95. http://dx.doi.org/10.1177/0954410016671343.

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A fluid–structure interaction numerical simulation was performed to investigate the flow field around a flexible flapping wing using an in-house developed computational fluid dynamics/computational structural dynamics solver. The three-dimensional (3D) fluid–structure interaction of the flapping locomotion was predicted by loosely coupling preconditioned Navier–Stokes solutions and non-linear co-rotational structural solutions. The computational structural dynamic solver was specifically developed for highly flexible flapping wings by considering large geometric non-linear characteristics. The
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3

Bhardwaj, Manoj K., Rakesh K. Kapania, Eric Reichenbach, and Guru P. Guruswamy. "Computational Fluid Dynamics/Computational Structural Dynamics Interaction Methodology for Aircraft Wings." AIAA Journal 36, no. 12 (1998): 2179–86. http://dx.doi.org/10.2514/2.342.

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Bhardwaj, Manoj K., Rakesh K. Kapania, Eric Reichenbach, and Guru P. Guruswamy. "Computational fluid dynamics/computational structural dynamics interaction methodology for aircraft wings." AIAA Journal 36 (January 1998): 2179–86. http://dx.doi.org/10.2514/3.14102.

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5

Wang, Ivan, and Earl H. Dowell. "Structural Dynamics Model of Multisegmented Folding Wings: Theory and Experiment." Journal of Aircraft 48, no. 6 (2011): 2149–60. http://dx.doi.org/10.2514/1.c031509.

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Wu, P., B. K. Stanford, E. Sällström, L. Ukeiley, and P. G. Ifju. "Structural dynamics and aerodynamics measurements of biologically inspired flexible flapping wings." Bioinspiration & Biomimetics 6, no. 1 (2011): 016009. http://dx.doi.org/10.1088/1748-3182/6/1/016009.

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7

Eberle, A. L., B. H. Dickerson, P. G. Reinhall, and T. L. Daniel. "A new twist on gyroscopic sensing: body rotations lead to torsion in flapping, flexing insect wings." Journal of The Royal Society Interface 12, no. 104 (2015): 20141088. http://dx.doi.org/10.1098/rsif.2014.1088.

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Insects perform fast rotational manoeuvres during flight. While two insect orders use flapping halteres (specialized organs evolved from wings) to detect body dynamics, it is unknown how other insects detect rotational motions. Like halteres, insect wings experience gyroscopic forces when they are flapped and rotated and recent evidence suggests that wings might indeed mediate reflexes to body rotations. But, can gyroscopic forces be detected using only changes in the structural dynamics of a flapping, flexing insect wing? We built computational and robotic models to rotate a flapping wing abo
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Zare, H., Seid H. Pourtakdoust, and A. Bighashdel. "Analytical structural behaviour of elastic flapping wings under the actuator effect." Aeronautical Journal 122, no. 1254 (2018): 1176–98. http://dx.doi.org/10.1017/aer.2018.74.

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ABSTRACTThe effect of inertial forces on the Structural Dynamics (SD) behaviour of Elastic Flapping Wings (EFWs) is investigated. In this regard, an analytical modal-based SD solution of EFW undergoing a prescribed rigid body motion is initially derived. The formulated initial-value problem is solved analytically to study the EFW structural responses, and sensitivity with respect to EFWs’ key parameters. As a case study, a rectangular wing undergoing a prescribed sinusoidal motion is simulated. The analytical solution is derived for the first time and helps towards a conceptual understanding o
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Otaki, Joji M. "Structural analysis of eyespots: dynamics of morphogenic signals that govern elemental positions in butterfly wings." BMC Systems Biology 6, no. 1 (2012): 17. http://dx.doi.org/10.1186/1752-0509-6-17.

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10

Kumar, David, Vemuri Shyam Kumar, Tigmanshu Goyal, P. M. Mohite, and S. Kamle. "Modal Analysis of Hummingbird Inspired MAV Flapping Wings." Applied Mechanics and Materials 772 (July 2015): 435–40. http://dx.doi.org/10.4028/www.scientific.net/amm.772.435.

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Natural flyers are the best source of inspiration for making successful MAVs. Hummingbirds are known for their excellent flight characteristics such as long duration hovering, backward flying, high agility, etc. Giant hummingbird is chosen as the bio-inspiration for designing the wing. Wings are required to be light, strong, and fatigue resistant to be used for MAV applications. Carbon nanotubes (CNTs)/Polypropylene (PP) composite is chosen as the wing membrane material whereas carbon fiber (CF)/epoxy (E) composite is chosen for wing frame. Two types of wings are fabricated, one is CNTs/PP win
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Dissertations / Theses on the topic "Wings (Anatomy) – Structural dynamics"

1

Preidikman, Sergio. "Numerical Simulations of Interactions Among Aerodynamics, Structural Dynamics, and Control Systems." Diss., Virginia Tech, 1998. http://hdl.handle.net/10919/30749.

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A robust technique for performing numerical simulations of nonlinear unsteady aeroelastic behavior is developed. The technique is applied to long-span bridges and the wing of a modern business jet. The heart of the procedure is combining the aerodynamic and structural models. The aerodynamic model is a general unsteady vortex-lattice method. The structural model for the bridges is a rigid roadbed supported by linear and torsional springs. For the aircraft wing, the structural model is a cantilever beam with rigid masses attached at various positions along the span; it was generated with the NA
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2

Bhardwaj, Manoj K. "A CFD/CSD Interaction Methodology for Aircraft Wings." Diss., web access:, 1997. http://scholar.lib.vt.edu/theses/public/etd-91097-165322/etd-title.html.

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Ray, Cody W. "Modeling, control, and estimation of flexible, aerodynamic structures." Thesis, 2012. http://hdl.handle.net/1957/29477.

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Engineers have long been inspired by nature's flyers. Such animals navigate complex environments gracefully and efficiently by using a variety of evolutionary adaptations for high-performance flight. Biologists have discovered a variety of sensory adaptations that provide flow state feedback and allow flying animals to feel their way through flight. A specialized skeletal wing structure and plethora of robust, adaptable sensory systems together allow nature's flyers to adapt to myriad flight conditions and regimes. In this work, motivated by biology and the successes of bio-inspired, engineere
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Books on the topic "Wings (Anatomy) – Structural dynamics"

1

United States. National Aeronautics and Space Administration., ed. A CFD/CSD interaction methodology for aircraft wings: A dissertation ... National Aeronautics and Space Administration, 1997.

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2

United States. National Aeronautics and Space Administration., ed. Experimental measurement of structural power flow on an aircraft fuselage: Progress report, grant number NAG-1-685. Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations, 1989.

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Experimental measurement of structural power flow on an aircraft fuselage: Progress report no. 6, Jan.-June 1989. Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations, 1991.

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Identification of rotorcraft structural dynamics from flight and wind tunnel data: Final report covering the period February 1991 - August 1992, prepared under NASA-Ames agreement no. NAG 2-694 ... National Aeronautics and Space Administration, 1997.

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5

United States. National Aeronautics and Space Administration., ed. Parallel aeroelastic computations for wing and wing-body configurations: Annual report for the period of time July 1993-July 1994. MCAT Institute, 1994.

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Book chapters on the topic "Wings (Anatomy) – Structural dynamics"

1

Wu, Pin, Erik Sällström, Lawrence Ukeiley, et al. "An Integrated Experimental and Computational Approach to Analyze Flexible Flapping Wings in Hover." In Structural Dynamics, Volume 3. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9834-7_127.

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Conference papers on the topic "Wings (Anatomy) – Structural dynamics"

1

HAAS, DAVID, and INDERJIT CHOPRA. "Flutter of circulation control wings." In 29th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2345.

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2

Cesnik, Carlos, Dewey Hodges, and Mayuresh Patil. "Aeroelastic analysis of composite wings." In 37th Structure, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-1444.

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3

OYIBO, G. "Accurate dynamic theory for supermaneuverable aircraft wings." In 27th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1006.

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4

GURUSWAMY, G., and P. GOORJIAN. "Transonic aeroelasticity of wings with tip stores." In 27th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1007.

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HAAS, DAVID, and INDERJIT CHOPRA. "Aeroelastic characteristics of swept circulation control wings." In 28th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-920.

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6

WEISSHAAR, TERRENCE, and JONATHAN BOHLMANN. "Supersonic flutter of aeroelastically tailored oblique wings." In 28th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-734.

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7

KANDIL, OSAMA, and H. CHUANG. "Unsteady flow computation of oscillating flexible wings." In 31st Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-937.

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8

BLAIR, M., and M. WILLIAMS. "A time domain panel method for wings." In 30th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1323.

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9

MEIROVITCH, L., and T. SEITZ. "Structural Modeling of Low-Aspect Ratio Composite Wings." In 34th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1371.

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GREEN, J. "Aeroelastic tailoring of composite wings with external stores." In 27th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1021.

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