Wing root (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Wing root" in English language version.

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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.

airspacemag.com

Garrison, Peter (February 2019). "The Perfect Airplane Wing". Air & Space Magazine.

archive.org

https://archive.org/details/the-cambridge-aerospace-dictionary, p.712

cambridge.org

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.

doi.org

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.
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.
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.

dtic.mil

apps.dtic.mil

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.

patents.google.com

researchgate.net

Ibrahim Halil Guzelbey; Yüksel Eraslan; Mehmet Hanifi Doğru (March 2019). "Effects of Taper Ratio on Aircraft Wing Aerodynamic Parameters: A Comperative Study".

ryerson.ca

digital.library.ryerson.ca

Yousefirad, Behzad (January 1, 2005). "Fatigue response of aircraft wing root joints under limit cycle oscillations". Ryerson University.

sciencedirect.com

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.

semanticscholar.org

api.semanticscholar.org

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.
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.

uq.edu.au

espace.library.uq.edu.au

Schwarz, Arman (2014). "Experimental Study of Hypersonic Wing/Fin Root Heating at Mach 8". University of Queensland.

utdallas.edu

personal.utdallas.edu

"Wing Root Fairings". utdallas.edu. Retrieved June 16, 2020.

web.archive.org

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.