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Titlebook: Contributions to the Development of Gasdynamics; Selected Papers, Tra Klaus Oswatitsch,Wilhelm Schneider,Max Platzer Book 1980 Springer Fac

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Theoretical Work about Transonic Flow at the Aeronautical Institute of the Royal Technical Universit., but the Institute has certain refinements to this case on its program of activities. There is a well-founded prospect to use the two extreme cases of large (infinite) and small aspect ratio to obtain results for the case of medium aspect ratio by interpolation.
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Aerodynamic Similarity at Axisymmetric Transonic Flow around Slender Bodiesmach number values are not similar, but are obtained from one another by transformation by means of a formula containing the second order derivative of the variable cross-section area along the body. Application to slightly supersonic flow around slender cones shows good agreement with exact theory.
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Calculation of Irrotational Axisymmetric Supersonic Flowfieldsrather large body apex angles. Further, one gets a new exact method, which is superior to the older methods with respect to accuracy and rapidity of execution, particularly in the domain of moderate supersonic velocities. A comparison with the experiments and with the linear method shows a wide applicability of the latter method.
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On the Representation of Flows in the Vicinity of Distinct Pointsntersection of shock waves and the reflection of shocks on the walls. In the mathematical sense, the shock equations really represent just a boundary condition for the flow properties on both sides of the shock front.
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Mechanics of Continua-A Brief Review,igator. One should expect that one ought to be able to find regular procedures, as is the case with the exact methods. Nevertheless, there will, of course, always be areas where estimates are difficult or impossible. As an example in the field of hydrodynamics, the stability of laminar flow might be mentioned.
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