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

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滋养

Aerodynamic Similarity at Axisymmetric Transonic Flow around Slender Bodiesnumber to retain the pressure distribution form, have already been derived. In the present report the corresponding similarity laws for slender bodies of revolution are derived. The form of these laws is such that the pressure distributions for bodies with affined relative thickness and free-stream

清澈

Similarity Laws for Hypersonic FlowSimilarity laws for this region were first derived by .. In the present report a different approach involving the shock wave equations is used. It is found that the pressure coefficients and lift forces are obtained, for hypersonic speeds, independent of the free stream Mach number and in the case o

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残忍

北极人

Ruptured-Disk

The Velocity Distribution on Symmetric Profiles with Local Supersonic Flow Regionswing and body. The characteristics of sub- and supersonic flow are so fundamentally different that it makes the identification of the sonic velocity decisively important, both in the experimental determination of drag, lift and pressure-point-location as well as in calculation methods. The theoretic

吃掉

The Flow around Bodies of Revolution at Mach Number 1ion method. For the transonic flow around smooth bodies of revolution the integral equation method seemed to be most suitable, but attempts with this method were quite disappointing. The sources and sinks produced by the effect of compressibility in the neighborhood of a body of revolution play only

外来

Calculation of Irrotational Axisymmetric Supersonic Flowfieldsnt, the v-component multiplied by y. For the procedure in the most general form, the product .. is decisive as the second independent variable. With such a combination of variables, one obtains very simple, rapidly working methods for slender bodies in the transonic range, which are also useful for

散步

On the Representation of Flows in the Vicinity of Distinct Pointsa wall, by sharp tips of bodies, by leading edges of plates in viscous or inviscid flow and by similar conditions. Likewise, the boundary conditions at infinity, for example the stipulation of the transition into a parallel flow, can lead to related problems. Finally, one needs to mention also the i