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Wing root
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<h2 id="see-also">See also</h2> <ul><li><a href="/facts/Wingbox/KcypKm4m">Wingbox</a></li></ul> <h2 id="external-links">External links</h2> <ul><li> Media related to Wing root at Wikimedia Commons</li></ul> <h2 id="references">References</h2> <ol> <li id="fn:1"><p>Peppler, I.L.: From The Ground Up, page 9. Aviation Publishers Co. Limited, Ottawa Ontario, Twenty Seventh Revised Edition, 1996. ISBN 0-9690054-9-0 <a href="/wiki/ISBN_(identifier)" target="_blank">/wiki/ISBN_(identifier)</a> <a href="#fnref:1" class="footnote-back-ref">↩</a></p></li> <li id="fn:2"><p>https://archive.org/details/the-cambridge-aerospace-dictionary, p.712 <a href="https://archive.org/details/the-cambridge-aerospace-dictionary" target="_blank">https://archive.org/details/the-cambridge-aerospace-dictionary</a> <a href="#fnref:2" class="footnote-back-ref">↩</a></p></li> <li id="fn:3"><p>Ibrahim Halil Guzelbey; Yüksel Eraslan; Mehmet Hanifi Doğru (March 2019). "Effects of Taper Ratio on Aircraft Wing Aerodynamic Parameters: A Comperative Study". <a href="https://www.researchgate.net/publication/328916819" target="_blank">https://www.researchgate.net/publication/328916819</a> <a href="#fnref:3" class="footnote-back-ref">↩</a></p></li> <li id="fn:4"><p>"US2927749A: Airfoil wing root fillet". 1956. <a href="https://patents.google.com/patent/US2927749A/en" target="_blank">https://patents.google.com/patent/US2927749A/en</a> <a href="#fnref:4" class="footnote-back-ref">↩</a></p></li> <li id="fn:5"><p>Garrison, Peter (February 2019). "The Perfect Airplane Wing". Air & Space Magazine. <a href="https://www.airspacemag.com/flight-today/perfect-airplane-wing-180971225/" target="_blank">https://www.airspacemag.com/flight-today/perfect-airplane-wing-180971225/</a> <a href="#fnref:5" class="footnote-back-ref">↩</a></p></li> <li id="fn:6"><p>"Wing Root Fairings". utdallas.edu. Retrieved June 16, 2020. <a href="https://personal.utdallas.edu/~klaus/Airplane/wing_root_fairing.html" target="_blank">https://personal.utdallas.edu/~klaus/Airplane/wing_root_fairing.html</a> <a href="#fnref:6" class="footnote-back-ref">↩</a></p></li> <li id="fn:7"><p>"US6152404A: Apparatus for influencing a wing root airflow in an aircraft". 1997. <a href="https://patents.google.com/patent/US6152404" target="_blank">https://patents.google.com/patent/US6152404</a> <a href="#fnref:7" class="footnote-back-ref">↩</a></p></li> <li id="fn:8"><p>Sobieczky, H (1998). "Configuration test cases for aircraft wing root design and optimization". Inverse Problems in Engineering Mechanics. International Symposium on Inverse Problems in Engineering Mechanics. pp. 371–380. doi:10.1016/B978-008043319-6/50043-1. ISBN 978-0-08-043319-6. <a href="978-0-08-043319-6" target="_blank">978-0-08-043319-6</a> <a href="#fnref:8" class="footnote-back-ref">↩</a></p></li> <li id="fn:9"><p>Large, E (March 1981). "The optimal planform, size and mass of a wing". The Aeronautical Journal. 85 (842). Cambridge University Press: 103–110. doi:10.1017/S0001924000029481. S2CID 116825025. <a href="https://www.cambridge.org/core/journals/aeronautical-journal/article/optimal-planform-size-and-mass-of-a-wing/8FC756BF2D248BFD9AD12AED9881D0A9" target="_blank">https://www.cambridge.org/core/journals/aeronautical-journal/article/optimal-planform-size-and-mass-of-a-wing/8FC756BF2D248BFD9AD12AED9881D0A9</a> <a href="#fnref:9" class="footnote-back-ref">↩</a></p></li> <li id="fn:10"><p>Yousefirad, Behzad (January 1, 2005). "Fatigue response of aircraft wing root joints under limit cycle oscillations". Ryerson University. <a href="https://digital.library.ryerson.ca/islandora/object/RULA%3A664" target="_blank">https://digital.library.ryerson.ca/islandora/object/RULA%3A664</a> <a href="#fnref:10" class="footnote-back-ref">↩</a></p></li> <li id="fn:11"><p>Lindauer, Jason M. (June 2010). "F/A-18(A-D) Wing Root Fatigue Life Expended (FLE) Prediction without the use of Stain Gage Data" (PDF). Naval Postgraduate School. Archived (PDF) from the original on December 1, 2020. <a href="https://apps.dtic.mil/dtic/tr/fulltext/u2/a524711.pdf" target="_blank">https://apps.dtic.mil/dtic/tr/fulltext/u2/a524711.pdf</a> <a href="#fnref:11" class="footnote-back-ref">↩</a></p></li> <li id="fn:12"><p>Waruna Seneviratne; John Tomblin; Gayanath Aponso; Travis Cravens; Madan Kittur; Anisur Rahman (September 2011). "Durability and Residual Strength Assessment of F/A-18 A-D Wing-Root Stepped-Lap Joint". AIAA Centennial of Naval Aviation Forum "100 Years of Achievement and Progress". Aerospace Research Centre. doi:10.2514/6.2011-7032. ISBN 978-1-62410-134-2. S2CID 111712573. <a href="978-1-62410-134-2" target="_blank">978-1-62410-134-2</a> <a href="#fnref:12" class="footnote-back-ref">↩</a></p></li> <li id="fn:13"><p>Schwarz, Arman (2014). "Experimental Study of Hypersonic Wing/Fin Root Heating at Mach 8". University of Queensland. <a href="https://espace.library.uq.edu.au/view/UQ:347730" target="_blank">https://espace.library.uq.edu.au/view/UQ:347730</a> <a href="#fnref:13" class="footnote-back-ref">↩</a></p></li> </ol>