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On the inlet vortex systemThe flow field of a jet engine with an inlet vortex, which can pick up heavy debris from the ground and damage the engine, was simulated in a small water tunnel by means of the hydrogen bubble technique. It was found that the known engine inlet vortex is accompained by a vortex system, consisting of two inlet vortices (the ground based and the trailing one), secondary vortices, and ground vortices. Simulation of the ground effect by an inlet image proved that the inlet vortex feeds on free stream vorticity and can exist without the presence of a ground boundary layer. The structural form of the inlet vortex system was explained by a simple potential flow model, which showed the number, location, and the importance of the stagnation points. A retractable horizontal screen or an up-tilt of the engine is suggested as countermeasure against debris ingestion.
Document ID
19740027081
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bissinger, N. C.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Braun, G. W.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-140182
Report Number: NASA-CR-140182
Accession Number
74N35194
Funding Number(s)
CONTRACT_GRANT: NGR-43-001-086
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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