Comparison of the aerodynamic performance of NACA 4415 and KFm based stepped airfoils

Author:

Kabir Asif,Akib Yeasir Mohammad,Hasan Mahdi,Islam Md. Jahirul

Publisher

AIP Publishing

Reference15 articles.

1. Abbott, I.H. and Von Doenhoff, A.E., 2012, Theory of wing sections: including a summary of airfoil data. Courier Corporation.

2. Wlezien, R.W., Horner, G.C., McGowan, A.R., Padula, S.L., Scott, M.A., Silcox, R.J., and Simpson, J.O., 1998. The aircraft morphing program. In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit (p. 1927).

3. Kasper, W.A., 1975. Some ideas of vortex lift (No. 750547). SAE Technical Paper.

4. Kruppa, E.W., 1977, January. A wind-tunnel investigation of the kasper vortex concept. In AIAA (pp. 77–310).

5. Davereap, “https://www.flitetest.com/articles/kfm-wings-a-basic-explanation.”

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