×

Wave drag of slender star-shaped bodies at moderate supersonic flight velocities. (English. Russian original) Zbl 0603.76063

Fluid Dyn. 18, 783-788 (1983); translation from Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza 1983, No. 5, 146-151 (1983).
The wave drag of star-shaped bodies at moderate supersonic flight velocities is discussed using an expression for slender sharp-pointed bodies that leads to a two-dimensional boundary value problem.
The main equation describing the wave drag is taken over from the quoted literature. Polar coordinates are introduced as well as an approximate potential function which is connected to an other function by the Cauchy- Riemann conditions. Some transformations are carried out, especially a conformal mapping of the interior of the unit disk onto the exterior of the n-ray star.
A Dirichlet problem is formulated for a complex potential, a term of which can be expressed by means of a Poisson integral, which however diverges at a certain point. Differentiation and the use of the Lagrangian formula finally leads to the solution of the Dirichlet problem mentioned above.
There occur infinite sums which contain Euler’s psi function and Euler’s constant. It is shown, that the several terms of the wave drag expression either belong to an axisymmetric part or to a nonaxisymmetric one.
The physical meaning of the solution parameters is discussed in detail. For instance the wave drag depends on the number of rays and on their shape. Best results within the family of star-shaped bodies discussed gives a five-point start with thin rays.
Reviewer: J.T.Heynatz

MSC:

76J20 Supersonic flows
Full Text: DOI

References:

[1] G. G. Chernyi and A. L. Gonor, ?The determination of body shapes of minimum drag using the Newton and the Busemann pressure laws,? Paper Presented at the Symposium on External Problems in Aerodynamics, Boeing Research Laboratories, Seattle, Washington (1962), p. 23.
[2] A. L. Gonor, ?Three-dimensional bodies of least drag at high supersonic velocities,? Prikl. Mat. Mekh.,27, 185 (1963).
[3] A. Miele (ed.), Theory of Optimum Aerodynamic Shapes, Academic Press (1965). · Zbl 0265.76076
[4] A. L. Gonor, M. A. Zubin, and N. A. Ostapenko, ?Experimental investigation of aerodynamic characteristics of star-shaped bodies at supersonic velocities,? in: Nonequilibrium Gas Flows and Optimal Body Shapes in Supersonic Flight [in Russian], Izd. MGU, Moscow (1978), pp. 28-39
[5] V. I. Lapygin, ?Calculation of supersonic flow over V-shaped wings by the method of stabilization,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 180 (1971). · Zbl 0218.76072
[6] V. I. Lapygin and N. A. Ostapenko, ?Supersonic gas flow over the windward side of a conical wing,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1, 112 (1973).
[7] V. I. Lapygin, ?Solution to the problem of flow over a V-shaped wing with strong shock wave on the leading edge,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 114 (1973). · Zbl 0269.76042
[8] G. N. Ward, ?Supersonic flow past slender pointed bodies,? Q. J. Mech. Appl. Math.,2, 75 (1949). · Zbl 0034.11705 · doi:10.1093/qjmam/2.1.75
[9] M. I. Follé, ?Linear theory of supersonic flow past ribbed bodies of three-dimensional configuration,? Izv. Akad. Nauk SSSR, Mekh, Zhidk. Gaza, No. 4, 94 (1978).
[10] M. A. Lavrent’ev and B. V. Shabat, Methods of the Theory of Functions of a Complex Variable [in Russian], Nauka, Moscow (1973), p. 736.
[11] V. I. Vasil’chenko, ?Optimal shapes of bodies of revolution in a linearized supersonic flow,? Tr. TsAGI, No. 1666, 20 (1975).
[12] A. Ferri, N. Ness, and T. T. Kaplita, ?Supersonic flow over conical bodies without axial symmetry,? J. Aeronaut, Sci.,20, 563 (1953). · Zbl 0050.41501
This reference list is based on information provided by the publisher or from digital mathematics libraries. Its items are heuristically matched to zbMATH identifiers and may contain data conversion errors. In some cases that data have been complemented/enhanced by data from zbMATH Open. This attempts to reflect the references listed in the original paper as accurately as possible without claiming completeness or a perfect matching.