جذر الجناح (Arabic Wikipedia)

Analysis of information sources in references of the Wikipedia article "جذر الجناح" in Arabic language version.

refsWebsite

Global rank Arabic rank

9web.archive.org

1^st place

2patents.google.com

1,182^nd place

3,220^th place

2doi.org

2^nd place

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1archive.org

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3^rd place

1researchgate.net

120^th place

247^th place

1airspacemag.com

4,171^st place

4,625^th place

1utdallas.edu

low place

1sciencedirect.com

149^th place

233^rd place

1cambridge.org

305^th place

299^th place

1ryerson.ca

low place

1dtic.mil

833^rd place

1,051^st place

1aiaa.org

7,940^th place

low place

1uq.edu.au

3,558^th place

3,179^th place

aiaa.org

arc.aiaa.org

"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. سبتمبر 2011. DOI:10.2514/6.2011-7032. ISBN:978-1-62410-134-2.

airspacemag.com

Garrison، Peter (فبراير 2019). "The Perfect Airplane Wing". Air & Space Magazine. مؤرشف من الأصل في 2021-05-23.

archive.org

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

cambridge.org

Large، E (مارس 1981). "The optimal planform, size and mass of a wing". The Aeronautical Journal. ج. 85 ع. 842: 103–110. مؤرشف من الأصل في 2020-06-18.

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. ص. 371–380. DOI:10.1016/B978-008043319-6/50043-1. ISBN:9780080433196.
"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. سبتمبر 2011. DOI:10.2514/6.2011-7032. ISBN:978-1-62410-134-2.

dtic.mil

apps.dtic.mil

Lindauer، Jason M. (يونيو 2010). "F/A-18(A-D) Wing Root Fatigue Life Expended (FLE) Prediction without the use of Stain Gage Data" (PDF). Naval Postgraduate School. مؤرشف من الأصل (PDF) في 2020-12-01.

patents.google.com

"US2927749A: Airfoil wing root fillet". 1956. مؤرشف من الأصل في 2021-07-08.
"US6152404A: Apparatus for influencing a wing root airflow in an aircraft". 1997. مؤرشف من الأصل في 2021-05-23.

researchgate.net

"Effects of Taper Ratio on Aircraft Wing Aerodynamic Parameters: A Comperative Study". مارس 2019. مؤرشف من الأصل في 2022-06-29.

ryerson.ca

digital.library.ryerson.ca

Yousefirad، Behzad (1 يناير 2005). "Fatigue response of aircraft wing root joints under limit cycle oscillations". Ryerson University. مؤرشف من الأصل في 2021-05-23.

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. ص. 371–380. DOI:10.1016/B978-008043319-6/50043-1. ISBN:9780080433196.

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. مؤرشف من الأصل في 2022-03-14.

utdallas.edu

personal.utdallas.edu

"Wing Root Fairings". utdallas.edu. مؤرشف من الأصل في 2020-11-25. اطلع عليه بتاريخ 2020-06-16.

web.archive.org

"Effects of Taper Ratio on Aircraft Wing Aerodynamic Parameters: A Comperative Study". مارس 2019. مؤرشف من الأصل في 2022-06-29.
"US2927749A: Airfoil wing root fillet". 1956. مؤرشف من الأصل في 2021-07-08.
Garrison، Peter (فبراير 2019). "The Perfect Airplane Wing". Air & Space Magazine. مؤرشف من الأصل في 2021-05-23.
"Wing Root Fairings". utdallas.edu. مؤرشف من الأصل في 2020-11-25. اطلع عليه بتاريخ 2020-06-16.
"US6152404A: Apparatus for influencing a wing root airflow in an aircraft". 1997. مؤرشف من الأصل في 2021-05-23.
Large، E (مارس 1981). "The optimal planform, size and mass of a wing". The Aeronautical Journal. ج. 85 ع. 842: 103–110. مؤرشف من الأصل في 2020-06-18.
Yousefirad، Behzad (1 يناير 2005). "Fatigue response of aircraft wing root joints under limit cycle oscillations". Ryerson University. مؤرشف من الأصل في 2021-05-23.
Lindauer، Jason M. (يونيو 2010). "F/A-18(A-D) Wing Root Fatigue Life Expended (FLE) Prediction without the use of Stain Gage Data" (PDF). Naval Postgraduate School. مؤرشف من الأصل (PDF) في 2020-12-01.
Schwarz، Arman (2014). "Experimental Study of Hypersonic Wing/Fin Root Heating at Mach 8". University of Queensland. مؤرشف من الأصل في 2022-03-14.