Supersonic flow over an inclined wing of zero aspect ratio

An asymptotic expression is found for the lift distribution on a long, narrow, laminar wing, at incidence in a supersonic stream. The approximations of the linearized potential theory are used.

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[2]  K. Schwarzschild,et al.  Die Beugung und Polarisation des Lichts durch einen Spalt. I , 1901 .

[3]  J. Gunn.  Linearized supersonic aerofoil theory part I , 1947, Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences.