Hostname: page-component-848d4c4894-cjp7w Total loading time: 0 Render date: 2024-06-14T16:13:59.687Z Has data issue: false hasContentIssue false

The static pressure in a vortex core

Published online by Cambridge University Press:  04 July 2016

J. Dunham*
Affiliation:
Engine Research Dept, National Gas Turbine Establishment

Extract

Vortices are of interest in many situations in fluid mechanics. One type of vortex with which the gas turbine designer is concerned is the line vortex springing like a miniature tornado from a point on the ground (or from a nearby aircraft surface) and entering the engine intake. It is possible for these vortices to suck stones up into the engine (Refs. 1, 2) and also to reduce the compressor surge margin (Refs. 3, 4). They are unsteady, in that their point of origin wanders about and so does their point of entry into the intake. This unsteadiness makes it very difficult to measure them, and so far no one known to the author has reported measurements of ground vortex strength, in the course of several investigations of the phenomenon (Refs. 1-3, 5-8).

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1979 

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. Rodert, L. A. and Garrett, F. B. Ingestion of foreign objects into turbine engines by vortices, NACA TN 3330, 1955.Google Scholar
2. Glenny, D. E. Ingestion of debris into intakes by vortex action, NGTE R.307, 1968, ARC CP 1114.Google Scholar
3. Motycka, D. L. Ground vortex—limit to engine/reverser operation, ASME Paper 75-GT-3, 1975.Google Scholar
4. Mitchell, G. A. Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbo-jet stall margin, NACA TMX-3246, 1975.Google Scholar
5. Colehour, J. L. and Farquhar, B. W. Inlet vortex. Jnl Aircraft. Vol 8, No 1, p 39. 1971.Google Scholar
6. Motycka, D. L., Walter, W. A. and Muller, G. L. An analytical and experimental study of inlet ground vortices. AIAA Paper 73-1313, 1973.Google Scholar
7. Motycka, D. L. and Walter, W. A. An experimental investigation of ground vortex formation during reverse engine operation. AIAA Paper 75-1322, 1975.Google Scholar
8. Swainston, M. J. C. Vortex formation near the intakes to turbomachinery and duct systems. Proc. I.Mech.E, Vol. 188, p 597. 1974.Google Scholar
9. Chigier, N. A. and Corsiglia, V. R. Tip vortices— velocity distributions, NASA TM X-62087, 1971.Google Scholar
10. Corsiglia, V. R., Schwind, R. G. and Chigier, N. A. Rapid scanning three-dimensional hot wire anemometer surveys of wing tip vortices, Jnl. Aircraft, Vol 10, No 12, p 752, 1973.Google Scholar
11. Orloff, K. L. Trailing vortex wind-tunnel diagnostics with a laser velocimeter. Jnl. Aircraft, Vol 11, No 8, p 477, 1974.Google Scholar
12. Johansson, T. G., Jernquist, L. F., Karlsson, S. K. F. and Frossling, N. Athree-component laser-doppler velocimeter, AGARD CP 193, Paper 28, 1976.Google Scholar
13. Baker, G. R., Barker, S. J., Bofah, K. K. and Saffman, P. G. Laser anemometer measurements of trailing vortices in water Jnl Fluid Mechanics, Vol 65, Pt 2, p 325, 1974.Google Scholar
14. Newman, B. G. Flow in a viscous trailing vortex, Aero Quarterly, Vol 10, p 149, 1959.Google Scholar
15. Batchelor, G. K. Axial flow in trailing line vortices, Jnl. Fluid Mechanics, Vol 20, Pt 4, p 645, 1964.Google Scholar
16. Iversen, J. D. Correlation of turbulent trailing vortex decay data, Jnl. Aircraft, Vol 13, No 5, p 338, 1976.Google Scholar
17. Mason, W. H. and Marchman, J. F. Far field structure of an aircraft trailing vortex including effects of mass injection, NASA CR-62078, 1972.Google Scholar
18. Logan, A. J. Vortex velocity distributions at large downstream distances. Jnl. Aircraft, Vol 8, No 11, p 930, 1971.Google Scholar
19. Sinclair, P. C. Some preliminary dust devil measurements Monthly Weather Review, Vol 22, No 8, p 363, 1964.Google Scholar