Two-Dimensional Bow Shock Wave Detachment Distances

Author:

Bryant R. A. A.

Abstract

In the recent paper by Warren a summary was made of current data on two-dimensional bow shock wave detachment distances. It was shown that the experimental results of Griffith and Alperin, as well as the detachment distances computed by Vincenti and Wagoner, could be collapsed into a single curve by using Spreiter's Transonic Similarity Parameter. This has been confirmed by the present authors who have found that the experimental results for wedges obtained by Bryson also correlate favourably with the curve given by Warren (Fig. 3 of Ref. 4).The results of the foregoing workers have been for steady flow conditions. However, it has been noted by Lilleyet aliathat a steady shock wave pattern can be established in free flight only after steady motion has been maintained for a considerable (infinite) time. In general, the locus of detached bow shock waves depends on the time history of the motion whenever a body is accelerated from subsonic speed.

Publisher

Cambridge University Press (CUP)

Reference15 articles.

1. A Study of Transonic Gas Dynamics by the Hydraulic Analogy

2. Some Comments on Surface Contamination in Hydraulic Analogy Research;Bryant;Journal of the Aeronautical Sciences,1956

3. Some Aspects of Noise From Supersonic Aircraft

4. Recent Advances in the Knowledge of Transonic Air Flow

5. Vincenti W. G. and Wagoner C. B. (1952). Transonic Flow Past a Wedge Profile with Detached Bow Wave N.A.C.A. Report 1095, 1952.

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