Hypersonic Gas Flow Past a Flat Plate with a Sharp Leading Edge

Hypersonic Gas Flow Past a Flat Plate with a Sharp Leading Edge
Author: G. M. Poedintsev
Publisher:
Total Pages: 16
Release: 1969
Genre:
ISBN:

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The problem of hypersonic gas flow over a plane plate with a sharp leading edge is discussed. It is assumed that the gas is perfect with a constant specific heat ratio and that the plate is thermally insulated. The problem is solved theoretically on the basis of a model which makes use of the geometrical characteristics of the Navier-Stokes equations. (Author).

A Critical Assessment of the Problem of Sharp Leading Edge of a Flat Plate in Hypersonic Flow

A Critical Assessment of the Problem of Sharp Leading Edge of a Flat Plate in Hypersonic Flow
Author: Amolak C. Jain
Publisher:
Total Pages: 42
Release: 1964
Genre: Aerodynamics, Hypersonic
ISBN:

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The advent of vehicles, moving many times the velocity of sound makes it necessary to understand clearly the various phenomena occuring near the sharp leading edge of a flat plate. A few theoretical attempts to tackle this problem are made and several experiments are performed at various places. Unfortunately wide areas of disagree ment exist between the various theoretical investigations and experimental results. It is the purpose of the note to try to gather some useful information from the available literature on this subject and present some suggestions which might be useful or worth consideration in any future attempt of solving this problem. (Author).

The Sharp Leading Edge Problem in Hypersonic Flow

The Sharp Leading Edge Problem in Hypersonic Flow
Author: Hakuro Oguchi
Publisher:
Total Pages: 86
Release: 1960
Genre: Leading edges (Aerodynamics)
ISBN:

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In the present paper the problem of hypersonic viscous flow past a semi-infinite flat plate with a sharp leading edge is considered. The study is concerned primarily with the rarefied flow region close enough to the leading edge that there is no longer an inviscid layer but where the shock wave is still thin. The solution which is obtained is shown to approach a wedge-like flow near the leading edge with a straight induced shock wave.