Exact and Approximate Solutions of Two-Dimensional Oblique Shock Flow

Author:

LAITONE EDMUND V.1

Affiliation:

1. Cornell Aeronautical Laboratory,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference12 articles.

1. Keenan, Joseph H., and Kaye, Joseph, Thermodynamic springer-Verlag, Berlin, 1943. Properties of Air, pp.36, 58;John Wiley & Sons, Inc., New York, 1945. (Continued on page 58) plest case, this would result in the use of a rectangular wing with a flat lower surface (very common 10 years ago), b u t it is also likely to affect thickness distribution and surface curvature. Peculiar twists and nonuniform curvature will frequently be so difficult to form t h a t the wing incorporating t h e m m a y be so distorted when it comes out of the shop as to definitely indicate some simpler shape would have given better aerodynamic results. This manufacturing problem m u s t not be overlooked in choosing airfoils.

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1. Isentropic Irrotational Steady Plane Flow;Applied Mathematical Sciences;1976

2. Die strengen nichtlinearen Grundgleichungen des Schallfeldes. Schallausbreitung bei großen Amplituden;Die Grundlagen der Akustik;1954

3. Readers Forum;Journal of the Aeronautical Sciences;1953-03

4. Two-Dimensional Airfoils at Moderate Hypersonic Velocities;Journal of the Aeronautical Sciences;1952-09

5. A Study of Transonic Gas Dynamics by the Hydraulic Analogy;Journal of the Aeronautical Sciences;1952-04

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