Hostname: page-component-77c89778f8-vsgnj Total loading time: 0 Render date: 2024-07-16T12:03:43.811Z Has data issue: false hasContentIssue false

Circulation measurements and vortical structure in an inlet-vortex flow field

Published online by Cambridge University Press:  21 April 2006

H. W. Shin
Affiliation:
Massachusetts Institute of Technology, Cambridge, MA 02139
E. M. Greitzer
Affiliation:
Massachusetts Institute of Technology, Cambridge, MA 02139
W. K. Cheng
Affiliation:
Massachusetts Institute of Technology, Cambridge, MA 02139
C. S. Tan
Affiliation:
Massachusetts Institute of Technology, Cambridge, MA 02139
C. L. Shippee
Affiliation:
Massachusetts Institute of Technology, Cambridge, MA 02139

Abstract

An investigation has been conducted of the three-dimensional flow associated with the inlet-vortex phenomenon. Quantitative measurements were made of inlet– and trailing-vortex circulation and position. Flow visualization was used to obtain information on the overall structure of the vorticity field. It is shown that the inlet vortex and the trailing vortex have essentially equal and opposite circulation. In addition, the production of vorticity, due to vortex stretching, is the mechanism by which both of these are maintained. A limited parametric study was also conducted to define the circulation and position (in the inlet) of the inlet vortex, for parameters of practical engineering interest.

Type
Research Article
Copyright
© 1986 Cambridge University Press

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

Boles, M. A. & Stockman, N. O. 1977 Use of experimental separation limits in the theoretical design of V/STOL inlets AIAA Paper No. 77–878.
De Siervi, F., Viguier, H. C., Greitzer, E. M. & Tan, C. S. Mechanisms of inlet vortex formation. J. Fluid Mech. 124, 173207.
Lighthill, M. J. 1963 Attachment and separation in three-dimensional flow. In Laminar Boundary Layers (ed. L. Rosenhead), pp. 72–82. Oxford University Press.
Liu, W., Greitzer, E. M. & Tan, C. S. 1985 Surface static pressures in an inlet vortex flow field. Trans. ASME J: J. Engng Gas Turbines & Power 107, 387393Google Scholar
Maskell, E. C. 1955 Flow separation in three dimensions. RAE Report 2565.
Motycka, D. L. 1976 Ground vortex-limit to engine reverser operation. Trans. ASME J: J. Engng Gas Turbines & Power 98, 258266Google Scholar
Perry, A. E. & Tan, D. K. M. 1984 Simple three-dimensional vortex motions in coflowing jets and wakes. J. Fluid Mech. 141, 197231.Google Scholar
Schmidt, D. P. & Okiishi, T. H. 1977 Multistage axial-flow turbomachine wake production, transport and interaction. AIAA J. 15 (8), 1138–1145.Google Scholar
Shin, H. W. & Shippee, C. 1984 Quantitative investigation of inlet vortex flow field. MIT Gas Turbine Laboratory Report No. 179.
Stockman, N. O. & Fabrell, C. A. 1977 Improved computer programs for calculating potential flow in propulsion system inlets. NASA TM-13728.Google Scholar
Tobak, M. & Peake, D. J. 1982 Topology of three-dimensional separated flows. Ann. Rev. Fluid Mech. 14.Google Scholar
Younghans, J. L. & Paul, D. L. 1978 Considerations in inlet engine integration. In The Aerothermodynamics of Aircraft Gas Turbine Engines (ed. G. C. Oates), AFAPL-TR-78-52, Air Force Aero Propulsion Laboratory.