Relevant bibliographies by topics / Aerospace structures

Contents

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

Academic literature on the topic 'Aerospace structures'

Author: Grafiati
Published: 4 June 2021
Last updated: 23 February 2023

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Journal articles on the topic "Aerospace structures"

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Krebs, Neil E., and Eric W. Rahnenfuehrer. "Aerospace Application of Braided Structures." Journal of the American Helicopter Society 34, no. 3 (July 1, 1989): 69–74. http://dx.doi.org/10.4050/jahs.34.69.

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Springer, George S. "Aerospace Composites in Civil Structures." IABSE Symposium Report 92, no. 31 (January 1, 2006): 13–19. http://dx.doi.org/10.2749/222137806796168859.

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Hanuska, A. R., E. P. Scott, and K. Daryabeigi. "Thermal Characterization of Aerospace Structures." Journal of Thermophysics and Heat Transfer 14, no. 3 (July 2000): 322–29. http://dx.doi.org/10.2514/2.6548.

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Dorey, G., C. J. Peel, and P. T. Curtis. "Advanced Materials for Aerospace Structures." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 208, no. 1 (January 1994): 1–8. http://dx.doi.org/10.1243/pime_proc_1994_208_247_02.

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The role of materials in aerospace structures is discussed in terms of engineering performance, at affordable costs, for a variety of applications. Vehicle performance can be extended by improved materials performance and examples are given of new materials (alloys, polymer matrix composites, metal matrix composites and hybrid laminates), from the concept of new microstructures through development of new manufacturing processes to pilot scale production.
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Hiraoka, Koichi. "Weight Reduction of Aerospace Structures." Journal of the Society of Mechanical Engineers 96, no. 893 (1993): 285–89. http://dx.doi.org/10.1299/jsmemag.96.893_285.

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Abrate, Serge. "Soft impacts on aerospace structures." Progress in Aerospace Sciences 81 (February 2016): 1–17. http://dx.doi.org/10.1016/j.paerosci.2015.11.005.

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Jadhav, Prakash. "Passive Morphing in Aerospace Composite Structures." Key Engineering Materials 889 (June 16, 2021): 53–58. http://dx.doi.org/10.4028/www.scientific.net/kem.889.53.

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Attempts to add the advanced technologies to aerospace composite structures like fan blade have been on in recent times to further improve its performance. As part of these efforts, it has been proposed that the blade morph feasibility could be studied by building and optimizing asymmetric lay up of composite plies inside the blade which will help generate enough passive morphing between max cruise and climb conditions of the flight. This will have a direct efficiency (Specific Fuel Consumption) benefit. This research describes the various ideas that were tried using in house-developed lay-up
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Spottswood, S. Michael, Benjamin P. Smarslok, Ricardo A. Perez, Timothy J. Beberniss, Benjamin J. Hagen, Zachary B. Riley, Kirk R. Brouwer, and David A. Ehrhardt. "Supersonic Aerothermoelastic Experiments of Aerospace Structures." AIAA Journal 59, no. 12 (December 2021): 5029–48. http://dx.doi.org/10.2514/1.j060403.

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Baldelli, Dario H., and Ricardo S. Sanchez Pena. "Uncertainty Modeling in Aerospace Flexible Structures." Journal of Guidance, Control, and Dynamics 22, no. 4 (July 1999): 611–14. http://dx.doi.org/10.2514/2.7637.

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Rittweger, A., J. Albus, E. Hornung, H. Öry, and P. Mourey. "Passive Damping Devices For Aerospace Structures." Acta Astronautica 50, no. 10 (May 2002): 597–608. http://dx.doi.org/10.1016/s0094-5765(01)00220-x.

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Dissertations / Theses on the topic "Aerospace structures"

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Jenett, Benjamin (Benjamin Eric). "Digital material aerospace structures." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/101837.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Civil and Environmental Engineering, 2015.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 71-76).<br>This thesis explores the design, fabrication, and performance of digital materials in aerospace structures in three areas: (1) a morphing wing design that adjusts its form to respond to different behavioral requirements; (2) an automated assembly method for truss column structures; and (3) an analysis of the payload and structural performance requirements of space structure elements made f
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Spendley, Paul R. "Design allowables for composite aerospace structures." Thesis, University of Surrey, 2012. http://epubs.surrey.ac.uk/810072/.

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Recent developments in aircraft design have seen the Airbus A380 and the Boeing Dreamliner employ significant amounts of advanced composite materials. There is some thought however, und the motivation for this current work, that these materials continue to suffer a weight penalty. In this work tests required to generate design allowables which accommodate environmental effects and holes arc performed on Carbon/epoxy quasi-isotropic laminatcs. The test data is treated statistically to provide B-basis allowables for each specimen type and condition. It was seen that the notched specimens (coupon
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Hanuska, Alexander Robert Jr. "Thermal Characterization of Complex Aerospace Structures." Thesis, Virginia Tech, 1998. http://hdl.handle.net/10919/36617.

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Predicting the performance of complex structures exposed to harsh thermal environments is a crucial issue in many of today's aerospace and space designs. To predict the thermal stresses a structure might be exposed to, the thermal properties of the independent materials used in the design of the structure need to be known. Therefore, a noninvasive estimation procedure involving Genetic Algorithms was developed to determine the various thermal properties needed to adequately model the Outer Wing Subcomponent (OWS), a structure located at the trailing edge of the High Speed Civil Transport's (
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White, Caleb, and caleb white@rmit edu au. "Health Monitoring of Bonded Composite Aerospace Structures." RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2009. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20090602.142122.

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Airframe assemblers have long recognised that for a new aircraft to be successful it must use less fuel, have lower maintenance requirements, and be more affordable. One common tactic is the use of innovative materials, such as advanced composites. Composite materials are suited to structural connection by adhesive bonding, which minimises the need for inefficient mechanical fastening. The aim of this PhD project was to investigate the application of existing, yet immature Structural Health Monitoring (SHM) techniques to adhesively bonded composite aerospace structures. The PhD study focu
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Zhang, Haochuan. "Nonlinear aeroelastic effects in damaged composite aerospace structures." Thesis, Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/12150.

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Navarro, Zafra Joaquin. "Computational mechanics of fracture on advanced aerospace structures." Thesis, University of Sheffield, 2016. http://etheses.whiterose.ac.uk/16883/.

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In this thesis, the computational simulation of cracks in advanced composite structures subjected to biaxial loading is studied. A structural integrity analysis using the eXtended Finite Element Method (XFEM) is considered for simulating the crack behaviour of a chopped fibre-glass-reinforced polyester (CGRP) cruciform specimen subjected to a quasi-static tensile biaxial loading [99]. This is the first time this problem is accomplished for computing the stress intensity factors (SIFs) produced in the biaxially loaded area of the cruciform specimen. SIFs are calculated for infinite plates under
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Lam, Daniel F. "STRAIN CONCENTRATION AND TENSION DOMINATED STIFFENED AEROSPACE STRUCTURES." University of Akron / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=akron1145393262.

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Vishwanathan, Aditya. "Uncertainty Quantification for Topology Optimisation of Aerospace Structures." Thesis, University of Sydney, 2020. https://hdl.handle.net/2123/23922.

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The design and optimisation of aerospace structures is non-trivial. There are several reasons for this including, but not limited to, (1) complex problem instances (multiple objectives, constraints, loads, and boundary conditions), (2) the use of high fidelity meshes which impose significant computational burden, and (3) dealing with uncertainties in the engineering modelling. The last few decades have seen a considerable increase in research output dedicated to solving these problems, and yet the majority of papers neglect the effect of uncertainties and assume deterministic conditions. This
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Pozegic, Thomas R. "Nano-modified carbon-epoxy composite structures for aerospace applications." Thesis, University of Surrey, 2016. http://epubs.surrey.ac.uk/809603/.

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Carbon fibre reinforced plastics (CFRP) have revolutionised industries that demand high specific strength materials. With current advancements in nanotechnology there exists an opportunity to not only improve the mechanical performance of CFRP, but to also impart other functionalities, such as thermal and electrical conductivity, with the aim of reducing the reliance on metals, making CFRP attractive to many other industries. This thesis provides a comprehensive analysis of the nano-phase modification to CFRP by growing carbon nanotubes (CNTs) on carbon fibre (CF) and performing mechanical, el
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Sebastian, Christopher. "Towards the validation of thermoacoustic modelling in aerospace structures." Thesis, University of Liverpool, 2015. http://livrepository.liverpool.ac.uk/2012079/.

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The research presented in this thesis has been performed over the course of three years under funding from the European Office of the United States Air Force (EAORD) as a part of a long-term project to collect high quality data for the validation of computational mechanics models of thermoacoustic loading. The focus is on the adaptation of stereoscopic (3D) Digital Image Correlation for use in a combined thermal and high temperature measurements. To that end, a background is provided which highlights the current state of the art in high temperature, vibration experiments and data acquisition.
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Books on the topic "Aerospace structures"

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J, Loughlan, ed. Aerospace structures. London: Elsevier Applied Science, 1990.

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Craig, J. I. (James I.), 1942- and SpringerLink (Online service), eds. Structural analysis: With applications to aerospace structures. Dordrecht: Springer, 2009.

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American Institute of Aeronautics and Astronautics, ed. Morphing aerospace vehicles and structures. Chichester, West Sussex: John Wiley & Sons, 2012.

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Rowe, W. J. Prospects for intelligent aerospace structures. New York: AIAA, 1986.

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Valasek, John. Morphing aerospace vehicles and structures. Chichester, West Sussex: John Wiley & Sons, 2012.

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Valasek, John, ed. Morphing Aerospace Vehicles and Structures. Chichester, UK: John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781119964032.

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Thornton, Earl A. Thermal structures for aerospace applications. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

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American Institute of Aeronautics and Astronautics., ed. Standard space systems: Structures, structural components, and structural assemblies. Reston, VA: American Institute of Aeronautics and Astronautics, 2005.

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Kruckenberg, Teresa M. Resin Transfer Moulding for Aerospace Structures. Dordrecht: Springer Netherlands, 1998.

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Soovere, J. Aerospace structures technology damping design guide. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, 1985.

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Book chapters on the topic "Aerospace structures"

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Gialanella, Stefano, and Alessio Malandruccolo. "Alloys for Aircraft Structures." In Aerospace Alloys, 41–127. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-24440-8_3.

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Sabbagh, Harold A., R. Kim Murphy, Elias H. Sabbagh, John C. Aldrin, and Jeremy S. Knopp. "Applications to Aerospace Structures." In Computational Electromagnetics and Model-Based Inversion, 337–51. New York, NY: Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4419-8429-6_17.

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Millán, Javier San, and Iñaki Armendáriz. "Delamination and Debonding Growth in Composite Structures." In Springer Aerospace Technology, 63–88. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-04004-2_3.

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Henson, Grant. "Materials for Launch Vehicle Structures." In Aerospace Materials and Applications, 435–504. Reston ,VA: American Institute of Aeronautics and Astronautics, Inc., 2018. http://dx.doi.org/10.2514/5.9781624104893.0435.0504.

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Wanhill, R. J. H. "Fatigue Requirements for Aircraft Structures." In Aerospace Materials and Material Technologies, 331–52. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2143-5_16.

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Dwibedy, Kartikeswar, and Anup Ghosh. "Damage analysis of multi-layered composite structures." In Aerospace and Associated Technology, 202–5. London: Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-36.

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Peel, C. J. "Advances in Aerospace Materials and Structures." In Materials for Transportation Technology, 183–97. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2005. http://dx.doi.org/10.1002/3527606025.ch30.

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Vargas-Rojas, Erik. "Composite Sandwich Structures in Aerospace Applications." In Sandwich Composites, 293–320. Boca Raton: CRC Press, 2021. http://dx.doi.org/10.1201/9781003143031-15.

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Valasek, John. "Introduction." In Morphing Aerospace Vehicles and Structures, 1–10. Chichester, UK: John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781119964032.ch1.

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Schick, Justin R., Darren J. Hartl, and Dimitris C. Lagoudas. "Incorporation of Shape Memory Alloy Actuators into Morphing Aerostructures." In Morphing Aerospace Vehicles and Structures, 231–60. Chichester, UK: John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781119964032.ch10.

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Conference papers on the topic "Aerospace structures"

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Smith, Howard Wesley. "Aerospace Structures Supportability." In General Aviation Aircraft Meeting and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1989. http://dx.doi.org/10.4271/891058.

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MITCHELL, ALAN, SAMUEL BRYAN, and MARK HALL. "Design engineering technologies for aerospace vehicles." In 28th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-715.

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HADJRIA, RAFIK, and OSCAR D’ALMEIDA. "Structural Health Monitoring for Aerospace Composite Structures." In Structural Health Monitoring 2019. Lancaster, PA: DEStech Publications, Inc., 2019. http://dx.doi.org/10.12783/shm2019/32280.

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Ravindra, K. "Aerospace Structures Course Revisited." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-979.

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DAYTO, SECTION,. "EVOLUTION OF AIRCRAFT/AEROSPACE STRUCTURES AND MATERIALS SYMPOSIUM." In 26th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-834.

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SPAIN, CHARLES, THOMAS ZEILER, MICHAEL GIBBONS, DAVID SOISTMANN, PETER POZEFSKY, RAFAEL DEJESUS, and CYPRIAN BRANNON. "AEROELASTIC CHARACTER OF A NATIONAL AEROSPACE PLANE DEMOSTRATOR CONCEPT." In 34th Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1314.

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LEVINE, STANLEY. "Ceramics and ceramic matrix composites - Aerospace potential and status." In 33rd Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2445.

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Hopkins, Mark, Douglas Dolvin, Donald Paul, Estelle Anselmo, and Jeffrey Zweber. "Structures technology for future aerospace systems." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-1869.

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Ghorbani, K., T. Baum, K. Nicholson, and J. Ahamed. "Advances aerospace multifunctional structures with integrated antenna structures." In 2015 Asia-Pacific Microwave Conference (APMC). IEEE, 2015. http://dx.doi.org/10.1109/apmc.2015.7413065.

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Hanuska, A., E. Scott, and K. Daryabeigi. "Thermal characterization of aerospace structures." In 37th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-1053.

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Reports on the topic "Aerospace structures"

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Venkayya, Vipperla B. Aerospace Structures Design on Computers. Fort Belvoir, VA: Defense Technical Information Center, March 1989. http://dx.doi.org/10.21236/ada208811.

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Grandhi, Ramana V., and Geetha Bharatram. Multiobjective Optimization of Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, July 1992. http://dx.doi.org/10.21236/ada260433.

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Atluri, S. N. AASERT-Structural Integrity of Aging of Aerospace Structures and Repairs. Fort Belvoir, VA: Defense Technical Information Center, December 1996. http://dx.doi.org/10.21236/ada326704.

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Farhat, Charbel. Multidisciplinary Thermal Analysis of Hot Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, May 2010. http://dx.doi.org/10.21236/ada564851.

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Grandt, A. F., Farris Jr., Hillberry T. N., and B. H. Analysis of Widespread Fatigue Damage in Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, February 1999. http://dx.doi.org/10.21236/ada360820.

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Selvam, R. P., and Zu-Qing Qu. Adaptive Navier Stokes Flow Solver for Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, May 2004. http://dx.doi.org/10.21236/ada424479.

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Atwood, Clinton J., Thomas Eugene Voth, David G. Taggart, David Dennis Gill, Joshua H. Robbins, and Peter Dewhurst. Titanium cholla : lightweight, high-strength structures for aerospace applications. Office of Scientific and Technical Information (OSTI), October 2007. http://dx.doi.org/10.2172/922082.

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Soovere, J., and M. L. Drake. Aerospace Structures Technology Damping Design Guide. Volume 3. Damping Material Data. Fort Belvoir, VA: Defense Technical Information Center, December 1985. http://dx.doi.org/10.21236/ada178315.

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Ounaies, Zoubeida, Ramanan Krishnamoorti, and Richard Vaia. Active Nanocomposites: Energy Harvesting and Stress Generation Media for Future Multifunctional Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, June 2010. http://dx.doi.org/10.21236/ada547363.

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Selvam, R. P., ZU-Qing QU, Qun Zheng, and Uday K. Roy. Predicting the Nonlinear Response of Aerospace Structures Using Aeroelastic NS Solutions on Deforming Meshes. Fort Belvoir, VA: Defense Technical Information Center, November 2001. http://dx.doi.org/10.21236/ada399278.

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