Measurements of the Flow Field on a 15° Semi-Vertex Angle Blunt Cone at M=8.6-Reference-Cited by-同舟云学术

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Measurements of the Flow Field on a 15° Semi-Vertex Angle Blunt Cone at M=8.6

Published:1969-02 Issue:1 Volume:20 Page:88-98
ISSN:0001-9259
Container-title:Aeronautical Quarterly
language:en
Short-container-title:Aeronautical Quarterly

Author:

Wood N. B.

Abstract

SummaryMeasurements of the pitot pressure between the body and shock on a 15° semi-vertex angle, spherically blunted cone were made in the RARDE Hypersonic Gun Tunnel at a Mach number of 8·6. Using these measurements, together with the measured shock shape, the other flow field parameters were calculated. The results were compared with results of inviscid theoretical calculations for a similar cone at a Mach number of 10.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference8 articles.

1. Inviscid hypersonic flow past smooth symmetric bodies

2. Wilby P. G. The flow field about a hemisphere-cylinder body at a Mach number of 7·3. FFA (Stockholm) Report 92, 1962.

3. Cleary J. W. An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic Mach numbers. NASA TN D-2969, 1965.

4. NOSE BLUNTNESS EFFECTS ON CONE PRESSURE AND SHOCK SHAPE AT M EQUALS 8

5. Determination of stagnation temperatures in the RARDE hypersonic gun tunnel from streak camera measurements of flow velocity;Bowman;ARC Current Paper 929,1967

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