Hostname: page-component-78c5997874-94fs2 Total loading time: 0 Render date: 2024-11-09T15:39:27.525Z Has data issue: false hasContentIssue false

Shock wave reflection from supersonic sea-skimming — a first look

Published online by Cambridge University Press:  04 July 2016

G. M. Moss*
Affiliation:
Applied Mechanics Branch, The Royal Military College of Science

Extract

There is currently some interest in supersonic sea-skimming as a possible terminal phase for anti-ship guided weapons. The flight of a supersonic vehicle, close to a density interface, will produce an additional series of shock waves from the reflection of the shock waves generated by the vehicle from the interface. The angle of reflection of these shock waves will depend, interalia,on the slope of the surface upon which they are incident. Given a surface with a periodic positional displacement, such as would be produced by a train of surface waves, the variation in position of the reflected shocks, in relation to the generating vehicle, will also be periodic in nature. This coherent motion could produce periodically fluctuating forces and moments on the vehicle generating the incident shocks and these, in turn, could cause stability or control problems for the missile autopilot.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1981 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Massey, B. S. Mechanics of fluids, Van Nostrand. 1968.Google Scholar
2. A selection of tables for use in calculations of compressible airflow, Oxford University Press. 1952.Google Scholar
3. Schapiro, A. H. The dynamics and thermodynamics of compressible fluid flow, Ronald. 1953.Google Scholar
4. Moss, G. M. Shock wave reflection from supersonic seaskimming, RMCS TN AM98. June 1981.Google Scholar