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Techniques for supersonic turbojet noise reduction
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- Munday, D. (author)
- University of Cincinnati
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- Cuppoletti, Daniel (author)
- University of Cincinnati
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- Perrino, M. (author)
- University of Cincinnati
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- (creator_code:org_t)
- ISBN 9780791844670
- 2012
- 2012
- English.
- In: ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012; Copenhagen; Denmark; 11 June 2012 through 15 June 2012. - 9780791844670 ; 1, s. 51-56
- Conference paper (peer-reviewed)
Abstract
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- Observations and simulations are presented of a supersonic jet from a nozzle representative of high-performance military aircraft such as the Saab Gripen. The nozzle has a design Mach number of 1.56 and is examined at its design condition with a surrounding secondary flow at Mach numbers of 0.0, 0.1 and 0.3. Chevrons and internal fluidic injection by microjets each reduce the noise generated by the main jet. Copyright © 2012 by ASME.
Subject headings
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering (hsv//eng)
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- kon (subject category)
- ref (subject category)
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- Chalmers University of Technology
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