Techniques for supersonic turbojet noise reduction
Paper i proceeding, 2012

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.

Författare

D. Munday

University of Cincinnati

Daniel Cuppoletti

University of Cincinnati

M. Perrino

University of Cincinnati

Ephraim Gutmark

University of Cincinnati

Markus Olander Burak

Chalmers, Tillämpad mekanik, Strömningslära

Lars-Erik Eriksson

Chalmers, Tillämpad mekanik, Strömningslära

ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012; Copenhagen; Denmark; 11 June 2012 through 15 June 2012

Vol. 1 51-56

Ämneskategorier

Maskinteknik

DOI

10.1115/GT2012-68304

ISBN

978-079184467-0