Relevant bibliographies by topics / Wings, Canard

Contents

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

Academic literature on the topic 'Wings, Canard'

Author: Grafiati
Published: 4 June 2021
Last updated: 27 July 2025

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Journal articles on the topic "Wings, Canard"

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Lai, Wenduo. "The working principles of canard wings and its aerodynamic advantages and effects on aircraft." Applied and Computational Engineering 91, no. 1 (2024): 83–88. http://dx.doi.org/10.54254/2755-2721/91/20241080.

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Canard wings have gradually become more and more popular since the advent of the supersonic jet era, and research on the subject has become more detailed in order to be able to manoeuvre this pair of small wings more perfectly and effectively. This paper mainly studies the aerodynamic principle of the canard wings and the impact of its aerodynamic advantages on the efficacy and stealth performance of the aircraft under different aerodynamic stability and makes a comparative analysis with the horizontal tail. Through literature analysis and review as well as a small number of comparative analys
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Mochizuki, Saya, and Gouji Yamada. "Aerodynamic characteristics and flow field of delta wings with the canard." MATEC Web of Conferences 145 (2018): 03010. http://dx.doi.org/10.1051/matecconf/201814503010.

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Now, many kinds of explorations for outer planets have been proposed around the world. Among them Mars attracts much attention for future exploration. Orbiters and landers have been used for Mars exploration. Recently as a new exploration method, the usage of an airplane has been seriously considered and there are some development projects for Mars airplane. However, the airplane flying on the Earth atmosphere cannot fly on the Mars atmosphere, because atmospheric conditions are much different each other. Therefore, we focused on the usage of the airplane with unfolding wings for Mars explorat
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Kishi, Yuki, Risato Yashiro, and Masahiro Kanazaki. "Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method." Aerospace 10, no. 8 (2023): 717. http://dx.doi.org/10.3390/aerospace10080717.

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Forward-swept wings can be expected to be lower-boom planforms with similar amount of drag as backward-swept wings because of their good lift distributions. In this study, the equivalent area distribution of a ten-seater supersonic forward-swept wing aircraft with a canard was designed to obtain design knowledge for leading boom reduction. The equivalent area distribution of the aircraft was calculated by solving the compressible Euler equation. A feasible target equivalent area distribution was generated based on Darden’s method and compared with the equivalent area distribution. To achieve a
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Wei, Dechen, Zhiwei Shi, Xi Geng, and Haisong Ang. "Experimental investigation of wing-body rock with nonzero equilibrium roll angles." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 4 (2017): 771–82. http://dx.doi.org/10.1177/0954410017690551.

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To study wing-body rock, various tests were used for the canard-configuration models in the wind tunnel, including free rolling, disturbance on free rolling, static moment measurements, dynamic derivative measurements, smoke wire method and particle image velocimetry. The models also have a chine forebody, strake wings, main wings and a vertical tail. In the tests, the canard deflection angles are 0° and 20° relative to the axis of the body. First, the roll angle time histories were obtained by free rolling motion and disturbed motion; the results demonstrate that both canard-configuration mod
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., Sutrisno, Firdaus RS, Zainuri A, Sigit Iswahyudi, and Setyawan Bekti Wibowo. "Performance Analysis and Visualization of Canard and Fuselage Effects on Flow Patterns around a Straight-Body-Type-Fuselage (SBTF) Fighter Models with Experimental Method in Water Tunnel." Modern Applied Science 12, no. 10 (2018): 195. http://dx.doi.org/10.5539/mas.v12n10p195.

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Performance analysis and visualization of canard and fuselage effects on flow patterns around an SBTF fighter model have been conducted. An SBTF fighter model with an experimental method in a water tunnel would easily reveal visually the vortex dynamics phenomenon that occurred. Testing has been done, with some form of non-canard and canard aircraft in a water tunnel, on vortex dynamics and aerodynamic power on the aircraft model. The stream demonstration used a fluid speed of 0.1 m/s and Reynolds number 6.577x103 on a 1:110 scale model and measured using dye injection method with a print ink
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Buresti, G., G. Lombardi, and P. Petagna. "Wing pressure loads in canard configurations: a comparison between numerical results and experimental data." Aeronautical Journal 96, no. 957 (1992): 271–79. http://dx.doi.org/10.1017/s0001924000050417.

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SummaryA comparison between computed and experimental pressure distributions on straight and forward-swept wings placed in interference with a fore canard surface at M = 0·3 and Re ≈ 2·8x106 is presented. It is shown that a numerical code, based on a non-linear vortex lattice method and expressly developed for the analysis of interfering lifting surfaces, is capable, in spite of its simplicity, of very accurate predictions in all configurations which do not correspond to sufficiently high angles of attack and to a close interference between the fore wake and the wing surface. Furthermore, even
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Ito, Yuma, and Hidetsugu Iwashita. "Characteristics of Steady Aerodynamics and Aerodynamic Interactions between Wings of a Canard-Configuration WIG." Journal of the Japan Society of Naval Architects and Ocean Engineers 25 (2017): 63–75. http://dx.doi.org/10.2534/jjasnaoe.25.63.

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Iwashita, Hidetsugu, Satoshi Tanaka, Masateru Suenaga, and Yasuaki Doi. "A Study on the Aerodynamic Interaction of Wings and the Aerodynamic Properties of a Canard-Configuration WISES Flying over Still Water and Waves (Part 1)." Journal of the Society of Naval Architects of Japan 2003, no. 194 (2003): 31–46. http://dx.doi.org/10.2534/jjasnaoe1968.2003.194_31.

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Iwashita, Hidetsugu. "A Study on the Aerodynamic Interaction of Wings and the Aerodynamic Properties of a Canard-Configuration WISES Flying over Still Water and Waves (Part 2)." Journal of the Society of Naval Architects of Japan 2003, no. 194 (2003): 47–57. http://dx.doi.org/10.2534/jjasnaoe1968.2003.194_47.

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Shao, Lintao, Dawei Bie, Jinting Xuan, and Menglong Ding. "Study on the influence of canard setting angle and longitudinal position on the sonic boom of supersonic business jet." Journal of Physics: Conference Series 3041, no. 1 (2025): 012009. https://doi.org/10.1088/1742-6596/3041/1/012009.

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Abstract The aerodynamic layout design for reducing sonic boom intensity was a crucial technology in the development of supersonic business jets. The canard-wing configuration served as a strategic approach to achieving a low sonic boom for supersonic business jets. In this study, the near-field and far-field sonic boom calculation results of the model, as provided by SBPW2, were compared to verify the accuracy of the adopted sonic boom prediction method. A low-sonic-boom configuration featuring a canard wing was proposed for a supersonic business jet, and a comparative analysis was conducted
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Dissertations / Theses on the topic "Wings, Canard"

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Mazza, Joseph R. "An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-03172010-020720/.

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Kersh, John M. Jr. "Lift enhancement using close-coupled canard wing vortex interaction." Thesis, Monterey, California: Naval Postgraduate School, 1990. http://hdl.handle.net/10945/27612.

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Approved for public release; distribution is unlimited.<br>A wind-tunnel study to find the lift and drag characteristics of a low-aspect-ratio wingbody configuration from an angle of attack (AOA) of -8 to 50 degrees was conducted. A further study to find the comparative lift enhancement using the same wingbody with a close-coupled canard for wingbody angles of attack of 10, 22, 34, 40, and 48 degrees and canard deflection angles from -25 to 25 degrees was carried out. It was found that a properly-located canard enhanced the lift at all tested angles of attack, compared to the baseline wingbody
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Kersh, John M. "Lift enhancement using close-coupled canard/wing vortex interaction." Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA245152.

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Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, December 1990.<br>Thesis Advisor(s): Howard, Richard M. Second Reader: Schmidt, Louis V. "December 1990." Description based on title screen as viewed on March 31, 2010. DTIC Identifier(s): Aerodynamic Lift, Canard Configurations, Theses. Author(s) subject terms: Canard, Close-Coupled Canard, High Angle of Attack Aerodynamics, Vortex Interaction. Includes bibliographical references (p. 124-125). Also available in print.
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Foster, Bruce Wayne. "New Right, old Canada, an analysis of the political thought and activities of selected contemporary right-wing organizations." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp03/NQ56543.pdf.

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Wagner, Jan-Philipp N. E. "Reporting on right-wing populism : evolving journalistic roles and practice in Canada, Germany, and the United Kingdom." Thesis, University of British Columbia, 2017. http://hdl.handle.net/2429/62911.

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Over the last five years, many European and North American democracies have experienced a significant resurgence of populist politics. Mostly situated on the right side of the political spectrum, these movements, parties, and politicians combine a strong appeal to the people and anti-establishment rhetoric with nationalist and even xenophobic sentiments. In addition, right-wing populist politicians commonly develop an ambiguous relationship with political journalists: they attempt to use newsmaker as mouthpieces for their political message and as amplifiers of their popularity; but they also a
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Allan, Shawn S. "A study of high wind storms affecting Atlantic Canada, 1979-1995." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape11/PQDD_0003/MQ44114.pdf.

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Pereira, Natanael de Carvalho. "Desenvolvimento de um sistema de aumento de estabilidade longitudinal de uma aeronave com enflechamento negativo e canard, com ensaios em túnel de vento." Universidade de São Paulo, 2005. http://www.teses.usp.br/teses/disponiveis/18/18135/tde-18022016-094528/.

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As pesquisas modernas em aeronáutica envolvem a expansão dos envelopes de vôo, como resultado do desejo de melhorar a manobrabilidade e controlabilidade em operações táticas, e melhorar a segurança do vôo. Esses objetivos podem ser alcançados através do desenvolvimento de sistemas automáticos de controle de vôo. Os sistemas de controle aplicados a aeronaves podem ser desenvolvidos e simulados através de métodos computacionais. No entanto, existem imperfeições na simulação computacional por não se conseguir reproduzir algumas características do vôo real ou devido a simplificações no modelo mate
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Bellini, Camilla Bonatto. "Variabilidade de alta frequência temporal da clorofila-a e sua relação com o campo de ventos e marés no canal de São Sebastião/SP." Universidade de São Paulo, 2016. http://www.teses.usp.br/teses/disponiveis/21/21134/tde-24022017-113529/.

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Em ambientes costeiros, a variabilidade da biomassa de fitoplâncton é dirigida por forçantes físicas locais que apresentam distintas escalas temporais em ocorrência, intensidade e durabilidade. No canal de São Sebastião, ambiente advectivo, parte-se do pressuposto de que qualquer adição da biomassa de fitoplâncton não se deve ao crescimento local, mas ao transporte de células fitoplanctônicas movidas pelas correntes guiadas a ventos e marés. Dessa maneira, o objetivo central deste trabalho é analisar a variabilidade em alta frequência das variações da biomassa fitoplanctônica e investigar suas
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Culver, Aaron Magelius Riis. "Not all speeds are created equal: investigating the predictability of statistically downscaled historical land surface winds over central Canada." Thesis, 2012. http://hdl.handle.net/1828/3908.

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A statistical downscaling approach based on multiple linear-regression is used to investigate the predictability of land surface winds over the Canadian prairies and Ontario. This study's model downscales mid-tropospheric predictors (wind components and speed, temperature, and geopotential height) from reanalysis products to predict historical wind observations at thirty-one airport-based weather surface stations in Canada. The model's performance is assessed as a function of: season; geographic location; averaging timescale of the wind statistics; and wind regime, as defined by how var
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Malheiro, Helena Maria Pereira da Silva. "Estratégia e relacionamento em canais de distribuição de vinhos." Master's thesis, 2014. http://hdl.handle.net/1822/30567.

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Dissertação de mestrado em Marketing e Estratégia<br>Esta dissertação analisa o desenvolvimento de estratégias de distribuição e explica os relacionamentos gerados no seio dos canais de distribuição de vinhos portugueses no mercado doméstico. O objetivo principal passa por compreender diferentes formas de cooperação entre os atores do sector, tendo em conta os seus objetivos estratégicos e o modo como os membros dos canais de distribuição se articulam e relacionam entre si por forma a melhorar a sua capacidade de ação no mercado. Foi adotada uma metodologia qualitativa através de um méto
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Books on the topic "Wings, Canard"

1

Kehoe, M. W. An in-flight interaction of the X-29A canard and flight control system. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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Kehoe, M. W. An in-flight interaction of the X-29A canard and flight control system. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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Bergmann, A. Aerodynamische Untersuchungen über Interferenzeffekte an Entenkonfigurationen. Zentrum für Luft- und Raumfahrttechnik, Technische Universität Braunschweig, 1996.

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Kehoe, M. W. An in-flight interaction of the X-29A canard and flight control system. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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Satran, Dale R. Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration. Langley Research Center, 1986.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration. National Aewronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration. National Aewronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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M, Sliwa Steven, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Parametric study of a canard-configured transport using conceptual design optimization. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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Anderson, Seth B. A look at handling qualities of canard configurations. National Aeronautics and Space Administration, Ames Research Center, 1987.

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Center, Langley Research, ed. Low speed wind tunnel test of a propulsive wing/canard concept in the STOL configuration. National Aeronautics and Space Administration, Langley Research Center, 1987.

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Book chapters on the topic "Wings, Canard"

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Perry, Barbara, and Ryan Scrivens. "Permission to Hate in Canada." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_4.

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Perry, Barbara, and Ryan Scrivens. "Thinking About Right-Wing Extremism in Canada." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_1.

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Perry, Barbara, and Ryan Scrivens. "Tracing the History of Right-Wing Extremism in Canada." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_2.

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Perry, Barbara, and Ryan Scrivens. "Looking In: Group Dynamics of the Canadian Right-Wing Extremist Movement." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_3.

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Perry, Barbara, and Ryan Scrivens. "Resisting the Right: Countering Right-Wing Extremism in Canada." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_5.

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Perry, Barbara, and Ryan Scrivens. "Epilogue: The Trump Effect on Right-Wing Extremism in Canada." In Right-Wing Extremism in Canada. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-25169-7_6.

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Rutan, Gerard F. "Western Canada: The Winds of Alienation*." In Scholars, Missionaries, and Counter-Imperialists. Routledge, 2022. http://dx.doi.org/10.4324/9781003216513-4.

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Zhu, Dehai, Yinong Zhang, Huimin Zhao, Ban Wang, and Zhenghong Gao. "Adaptive Fault-Tolerant Control of a Canard Rotor/Wing VTOL Aircraft." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-6613-2_319.

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Lee, Jae-Woo, Kwon-Su Jeon, Min-Ji Kim, Yung-Hwan Byun, Chang J. Kim, and Yung H. Yu. "Rotor Design for the Performance Optimization of Canard Rotor/Wing Aircraft." In Computational Science and Its Applications - ICCSA 2006. Springer Berlin Heidelberg, 2006. http://dx.doi.org/10.1007/11751649_102.

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Thunert, Martin. "Conservative Think Tanks in the United States and Canada." In Conservative Parties and Right-Wing Politics in North America. VS Verlag für Sozialwissenschaften, 2003. http://dx.doi.org/10.1007/978-3-663-09508-8_11.

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Conference papers on the topic "Wings, Canard"

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Juhasz, Ondrej, and Jean-Paul Reddinger. "System Identification of a Hovering Quadrotor Biplane Tailsitter with Canted Motors." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1190.

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A quadrotor was modified by adding wings to the frame to directly compare the flight dynamics characteristics as well as the stability and control derivatives of the quadrotor and its biplane tailsitter variant. The on axis response of the quadrotor and a biplane tailsitter variant were measured through flight test and frequency domain system identification was used for non-parametric and parametric model identification. Identification of the full vehicle dynamics demonstrated that also identifying the motor torque and back-EMF constants from no-load measurements and the remaining motor parame
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Fardink, Paul. "Glenn Hammond Curtiss, the Aerial Experiment Association and the John Newton Williams Helicopter of 1908." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9520.

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The theme of the AHS 70th Annual Forum and Technology Display in Montréal, Québec, Canada, is "Celebrating International Cooperation in Vertical Flight Technology." Perhaps no finer example exists of this type of cooperation than with Alexander Graham Bell's Aerial Experiment Association, a Canadian-American aeronautical research group formed on October 1, 1907, at Baddeck, Nova Scotia. According to Bell, the A.E.A. was a "co-operative scientific association, not for gain but for the love of the art and for doing what we can to help one another," and dedicated to the construction of a practica
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Gibb, Keely, Navin Francis, Andrew Law, et al. "Methods for Laboratory Replication of Rotary-wing Air Ambulance Vibration Conditions for Neonatal Patient Transport Applications." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-71.

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Neonatal patients in need of specialized care may require transport by rotary-wing air ambulances. These patients are subjected to environmental stressors during transport, including elevated levels of mechanical vibration. Aircraft vibration is transmitted through the transport system and incubator to the patient. The unique vibration profile is dependent on vehicle model and phase of flight. To improve safety for these patients, we aim to evaluate the vibration exposure across this complex system. The purpose of this paper is to present and evaluate the methods used for aircraft data collect
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Klassen, R. D., and P. R. Roberge. "Passive Monitoring of Atmospheric Corrosives and Pollutants at Three CF Bases." In CORROSION 2002. NACE International, 2002. https://doi.org/10.5006/c2002-02149.

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Abstract Atmospheric corrosion rates are recognized to depend on the deposition rates of corrosives, such as salt aerosols, and pollutants, such as sulfur dioxide, as well as the relative humidity. The corrosivity at three Canadian Forces bases (CFB Greenwood, CFB Kingston and CFB Esquimalt) was measured with CLIMAT coupons on a monthly basis. Even though these bases are at opposite ends of Canada, each had a maximum corrosivity in the winter and a minimum corrosivity in the summer. This trend was consistent with the average speed of winds that were associated with a relative humidity greater
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Dikshit, Abhijnan, Tom Stokkermans, Shawn Lim, and James Wang. "Effect of Lifting Surface and Tail Configuration on the Aerodynamics and Flight Mechanics of VTOL Aircraft." In Vertical Flight Society 78th Annual Forum & Technology Display. The Vertical Flight Society, 2022. http://dx.doi.org/10.4050/f-0078-2022-17483.

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To increase the cruising range for VTOL aircraft it has become necessary to add a wing or wings so the aircraft can vertically take off like a helicopter but cruise like an airplane. This paper compares the aerodynamic efficiency, stability, and handling qualities of four different cruise configurations: conventional wing-tail airplane, canard airplane, flying wing and tandem wing. An additional aim is to perform a parametric study of the tandem wing aircraft configuration because that has become a popular choice among eVTOL aircraft designers. This paper does not examine the hovering flight p
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Ishibashi, Shojiro, Hiroshi Yoshida, Makoto Sugesawa, Yutaka Ohta, and Frank Hsiao Fan. "An AUV Yumeiruka for Seabed Topography Survey." In ASME 2015 34th International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/omae2015-41830.

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Japan Agency for Marine – Earth Science and Technology (JAMSTEC) has been recently advanced the development of several underwater vehicles for the survey of mineral resources buried under Japan’s territorial sea. One of them is Yumeiruka. It has characteristic canard wings and rudders which are attached on its fore and rear parts. Since they cause good maneuverability, good survey results using acoustic observation devices can be obtained. And it has a high performance compact inertial navigation system which was developed as Japan’s first INS for an underwater vehicle by the cooperation betwe
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Tu, Eugene. "Time-accurate Navier-Stokes simulation of a canard-wing-body configuration with moving canards." In 14th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2407.

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March, Andrew I., Charles W. Bradley, and Ephraim Garcia. "Aerodynamic Properties of Avian Flight as a Function of Wing Shape." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-83011.

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Presently, all man-made aircraft are optimized for one specific flight regime. Commercial aircraft fly at a specific cruising altitude at which they are most efficient, and military aircraft, which require excellent performance in many flight regimes are designed to be ‘good’ at all of them. A new concept in aviation, morphing aircraft, or aircraft that can fully change their shape, will allow for optimization at nearly any flight regime. This concept has been millennia in the making, well before mankind. Looking to various bird species, tails and wings can completely change shape to optimize
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TU, EUGENE. "Effect of canard deflection on close-coupled canard-wing-body aerodynamics." In 10th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2602.

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Tengfei Guo, Honglun Wang, and Wendong Gai. "Transition flight control for Canard Rotor/Wing rotorcraft." In 2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC). IEEE, 2011. http://dx.doi.org/10.1109/aimsec.2011.6010405.

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Reports on the topic "Wings, Canard"

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Journeay, M., P. LeSueur, W. Chow, and C L Wagner. Physical exposure to natural hazards in Canada. Natural Resources Canada/CMSS/Information Management, 2022. http://dx.doi.org/10.4095/330012.

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Natural hazard threats occur in areas of the built environment where buildings, people, and related financial assets are exposed to the physical effects of earth system processes that have a potential to cause damage, injuries, losses, and related socioeconomic disruption. As cities, towns, and villages continue to expand and densify in response to the pressures of urban growth and development, so too do the levels of exposure and susceptibility to natural hazard threat. While our understanding of natural hazard processes has increased significantly over the last few decades, the ability to as
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Levy Yeyati, Eduardo, Ernesto H. Stein, and Christian Daude. The FTAA and the Location of FDI? Inter-American Development Bank, 2003. http://dx.doi.org/10.18235/0009108.

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The role of regional integration agreements (RIAs) as a determinant of the location of Foreign Direct Investment (FDI) has become an increasingly relevant issue for emerging economies. While the concerns regarding the impact of RIAs on FDI for countries in Latin America may be related to a number of RIA initiatives of different types (sub regional South-South agreements, agreements with the EU, etc.), the largest effects are likely to be associated with the ( Free Trade Area of the Americas ) FTAA. In this regard, there are a number of highly relevant questions: For instance, what effect will
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3

Sandford, Robert, Vladimir Smakhtin, Colin Mayfield, et al. Canada in the Global Water World: Analysis of Capabilities. United Nations University Institute for Water, Environment and Health, 2018. http://dx.doi.org/10.53328/vsgg2030.

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This report critically examines, for the first time, the capacity of Canada’s water sector with respect to meeting and helping other countries meet the water-related targets of the UN’s global sustainable development agenda. Several components of this capacity are examined, including water education and research, investment in water projects that Canada makes internally and externally, and experiences in water technology and governance. Analysis of the water education system suggests that there is a broad capability in institutions of higher learning in Canada to offer training in the diverse
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4

Hodul, M., H. P. White, and A. Knudby. A report on water quality monitoring in Quesnel Lake, British Columbia, subsequent to the Mount Polley tailings dam spill, using optical satellite imagery. Natural Resources Canada/CMSS/Information Management, 2022. http://dx.doi.org/10.4095/330556.

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In the early morning on the 4th of August 2014, a tailings dam near Quesnel, BC burst, spilling approximately 25 million m3 of runoff containing heavy metal elements into nearby Quesnel Lake (Byrne et al. 2018). The runoff slurry, which included lead, arsenic, selenium, and vanadium spilled through Hazeltine Creek, scouring its banks and picking up till and forest cover on the way, and ultimately ended up in Quesnel Lake, whose water level rose by 1.5 m as a result. While the introduction of heavy metals into Quesnel Lake was of environmental concern, the additional till and forest cover scour
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