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7 References

[1] Chiarelli M. R., Cagnoni M., Ciabattari M., De Biasio M., Massai A., “High aspect ratio wing with curved planform: CFD and FE analyses”, 27th International Congress of the Aeronautical Sciences, Paper ID 452, CD-Rom Proceedings ISBN 978-0-9565333-0-2, Optimage Ltd, Edinburgh, UK, 2010.

[2] Chiarelli M. R., Cagnoni M., Ciabattari M., De Biasio M., Massai A., “Preliminary analysis of a high aspect ratio wing with curved planform”, XX AIDAA Congress, Milan, Italy, June 29–July 3, 2009.

[3] Chiarelli M.R., Lombardi G., Nibio A. “A straight wing and a forward swept wing compared with a curved planform wing in the transonic regime”, CEAS 2011, International Conference of the European Aerospace Societies, Venice, Italy, CD-Rom ISBN 978-88-96427-18-7, pp. 1175-1184, October 2011.

[4] Chiarelli M. R., Cagnoni M., Ciabattari M., Lombardi G.,” Fluid-Structure Interaction Analyses of Wings with Curved Planform: Preliminary Aeroelastic Results”, Aerospace Unit, Department of Civil and Industrial Engineering, University of Pisa, Italy, 2013

[5] Chiarelli M. R., Bonomo S. “Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s Influence on the Dynamic Instability”, Hindawi Publishing Corporation, International Journal of Aerospace Engineering, Volume 2016, Article ID 3563684 [6] Kwan S., “Numerical Research on ARARD 445.6 Wing Flutter Boundary: A

Comparison With Curved Planform Wing”, Master degree thesis in Aerospace Engineering, Pisa University, 2017.

[7] Küchemann D., The aerodynamic design of aircraft, Pergamon, London, 1978, ISBN 0-08- 020514-3, pp. 103-220.

[8] Jameson A., Ou K., “50 years of transonic aircraft design”, Aeronautics and Astronautics Department, StanfordUniversity, United States, Progress in Aerospace Sciences, Volume 47, Issue 5, July 2011, Pages 308-318

[9] Lock R. C., “Design of wing plan forms for transonic speeds”, The Aeronautical Quarterly, Royal Aeronautical Society, London, GB, Vol. 12, No. Part 1, 1961, pp. 65-93.

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[10] Van Dam C.P., Vijgen P.M.H.W., Holmest B.J., “Experimental Investigation on the Effect of Crescent Planform on Lift and Drag”, Journal of Aircraft, Vol. 28, No. 11, 1991, pp. 713-720.

[11] Ashenberg J., Weihs D., “Minimum Induced Drag of Wings with Curved Planform“, Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 89-91.

[12] Vaughn M. E., Burkhalter J. E., ”Pressure Loading on Curved Leading Edge Wings in Supersonic Flow”, Journal of Aircraft, Vol. 23, No. 7, 1986, pp. 574-581.

[13] Holdaway G. H. and Mellenthin J. A., “Evaluation of blended wing-body combinations with curved plan forms at mach numbers up to 3.50,” NASA 19980227180, 1960.

[14] Heller G. et all, “Wing Tip Extension for a Wing”, Pub. No. US2002162917A1, http://ep.espacenet.com/, 7 November 2002.

[15] NASA Common Research Model website: https://commonresearchmodel.larc.nasa.gov/

[16] Vassberg J. C., DeHaan M. A., Rivers S. M., Wahls R. A., “Development of a Common Research Model for applied CFD validation studies”, AIAA Paper 2008-6919, 26th AIAA Applied Aerodynamics Conference, Hawaii, HI, August 2008. [17] Vassberg J. C., Tinoco E. N., Mani M., Zickuhr T., Levy D. W., Brodersen O. P.,

Eisfeld B., Wahls R. A., Morrison J. H., Mavriplis D. J., Murayama M., “Summary of the Fourth AIAA CFD Drag Prediction Workshop”, AIAA Paper 2010-4547, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 2010.

[17] Oswald M., ANSYS Germany GmbH, 4th AIAA CFD Drag Prediction Workshop Presentation, 2009.

[18] Melissa B. Rivers, Craig A. Hunter and Richard L. Campbell NASA Langley Research Center, Hampton, VA 23681 “Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model”

[19] Vassberg J. C., “A Unified Baseline Grid about the Common Research Model Wing-Body for the Fifth AIAA CFD Drag Prediction Workshop”, AIAA Paper 2011-3508, Honolulu, Hawaii, June 2011.

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