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An experimental investigation of supersonic swirling jetsThe addition of swirl to scramjet fuel jets has been proposed as a method of enhancing fuel mixing, but little of a fundamental nature is known about supersonic swirling flows. This is a study of mixing in supersonic swirling air jets created by tangential injection and acceleration through a convergent-divergent nozzle into stagnant air. Several cases with different vortex circulations were investigated using pitot, cone and total-temperature probes, and Rayleigh scattering from a laser light sheet. The results show that tangential injection is an efficient method for generating swirling jets; that the swirling jets mix much more rapidly with the ambient air than comparable straight jets; and that when overexpanded, considerable turbulence and increased mixing is created as a result of vortex breakdown.
Document ID
19930064126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cutler, Andrew D.
(George Washington Univ., Washington; NASA, Langley Research Center Hampton, VA, United States)
Levey, Brian S.
(NASA Langley Research Center Hampton, VA, United States)
Kraus, Donna K.
(George Washington Univ. Washington, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-2922
Meeting Information
Meeting: AIAA, Fluid Dynamics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
93A48123
Funding Number(s)
CONTRACT_GRANT: NAS1-18458
CONTRACT_GRANT: NCC1-24
Distribution Limits
Public
Copyright
Other

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