A Technique for Determining Relaxation Times by Free-Flight Tests of Low-Fineness-Ratio Cones; With Experimental Results for Air at Equilibrium Temperatures Up to 3440 K

A Technique for Determining Relaxation Times by Free-Flight Tests of Low-Fineness-Ratio Cones; With Experimental Results for Air at Equilibrium Temperatures Up to 3440 K

Author: Jack D. Stephenson

Publisher:

Published: 1960

Total Pages: 64

ISBN-13:

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This report describes a technique which combines theory and experiments for determining relaxation times in gases. The technique is based on the measurement of shapes of the bow shock waves of low-fineness-ratio cones fired from high-velocity guns. The theory presented in the report provides a means by which shadowgraph data showing the bow waves can be analyzed so as to furnish effective relaxation times. Relaxation times in air were obtained by this technique and the results have been compared with values estimated from shock tube measurements in pure oxygen and nitrogen. The tests were made at velocities ranging from 4600 to 12,000 feet per second corresponding to equilibrium temperatures from 35900 R (19900 K) to 6200 R (34400 K), under which conditions, at all but the highest temperatures, the effective relaxation times were determined primarily by the relaxation time for oxygen and nitrogen vibrations.


The High Temperature Aspects of Hypersonic Flow

The High Temperature Aspects of Hypersonic Flow

Author: Wilbur C. Nelson

Publisher: Elsevier

Published: 2014-12-02

Total Pages: 801

ISBN-13: 1483223310

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The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.


Hypersonic Inviscid Flow

Hypersonic Inviscid Flow

Author: Wallace D. Hayes

Publisher: Courier Corporation

Published: 2012-07-13

Total Pages: 628

ISBN-13: 0486160483

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Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.