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Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form
"The idea is advanced of making a supersonic nozzle by producing one, two, or three successive turns of the whole flow; with the result that the wall contour can be calculated exactly by means of the Prandtl-Meyer "Lost Solution" (p. 1).
Date:
January 1953
Creator:
Cunsolo, Dante
System:
The UNT Digital Library
Steady Vibrations of Wing of Circular Plan Form and Theory of Wing of Circular Plan Form
This paper treats the problem of determining the lift, moment, and induced drag of a thin wing of circular plan form in uniform incompressible flow on the basis of linearized theory. As contrasted to a similar paper by Kinner, in which the acceleration potential method was used, the present paper utilizes the concept of the velocity potential. Calculations of the lift and moment are presented for several deformed shapes.
Date:
January 1953
Creator:
Kochin, N. E.
System:
The UNT Digital Library