Add to ORKGThe original study of a conical body of circular cross section at zero angle of attack inside a supersonic flow was developed by Taylor & Maccoll 1933, see [1]. After this year a large amount of numerical and perturbation techniques were developed to approximate solutions and to deal with the problem.www.proceedings.blucher.com.br/evento/10wccmFil: Ferreyra, R. T. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas, Físicas y Naturales. Departamento de Matemática; Argentina.Fil: Tamagno, J. P. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas, Físicas y Naturales. Departamento de Aeronaútica; Argentina.Otras Ingenierías y Tecnología
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AbstractThis paper studies the steady supersonic flow past a Lipschitz curved cone. Under the assump...
Any analytical closed-form solution can offer a deep insight into understanding the fundamentals of ...
An approximate closed form solution to the internal conical, hypersonic flow about a circular cone a...
In this technical note, we present an asymptotic approximation for supersonic flow about a pointed c...
An analysis of inviscid, compressible flow over a porous conne or wedge is given where the body is i...
The inverse method, with the shock wave prescribed to be an elliptic cone at a finite angle of incid...
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The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
The technique of floating shock fitting is adapted to the computation of the inviscid flowfield abou...
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1AbstractCurved shock theory (CST) has been extended to apply to axisymmetric shocks in non-uniform ...
Flows of relevance to new generation aerospace vehicles exist, which are weakly dependent on the str...
By applying hyper sonic approximations to Ferri's linearized characteristics method simple re suits...
AbstractThis paper studies the steady supersonic flow past a Lipschitz curved cone. Under the assump...