Lift-Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight-Tapered Wings

Author： M.I.A.S. A. Stanbrook   B.Sc.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.26, Iss.8, 1993-12, pp. : 244-257

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

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