Abstract
PIV measurements were performed to provide insight into the effect of serrated (chevron) nozzles on the flow field of a coaxial circular jet. The serrations were tested on the primary nozzle. Mean flow results showed that the chevron effectively redistributes momentum from the high velocity center stream outward to the lower velocity secondary stream by creating lateral jets. This leads to a more rapid decay of the peak jet velocity and a consequent reduction in the length of the jet potential core. Local increases of up to 65% in the outer stream velocity were measured. The interaction of the secondary jets with the lower velocity outer stream produces increases in turbulent kinetic energy (TKE) near the center nozzle lip. These flow field effects correlate with the jet’s acoustic emissions: Reduction of low-frequency noise due to large scale mixing and potential core shortening, and increased high-frequency noise due to increased near-field turbulence.
Similar content being viewed by others
Abbreviations
- A :
-
Cross sectional area
- M :
-
Jet exhaust Mach number
- \( \mathop m\limits^{ \cdot } \) :
-
Mass flow rate
- N :
-
Number of chevron lobes
- NPR:
-
Nozzle pressure ratio
- T :
-
Temperature
- TKE:
-
Turbulent kinetic energy
- V :
-
Jet exhaust velocity
- V shear :
-
Nozzle shear velocity (V p − V s)
- V mix :
-
Nozzle mixed velocity
- u′:
-
Axial turbulence component
- v′:
-
Radial turbulence component
- j:
-
Lateral/secondary jet (or lobe)
- o:
-
Total or stagnation property
- p:
-
Primary flow
- s:
-
Secondary flow
References
Ahuja KK, Brown WH (1989) Shear flow control by mechanical tabs, AIAA-89-0994
Ahuja KK, Manes JP, Massey KC (1990) An evaluation of various concepts of reducing supersonic jet noise, AIAA-90-3982
Bradbury LJS, Khadem AH (1975) The distortion of a jet by tabs. J Fluid Mech 70(4):801–813
Bridges J, Wernet MP (2002) Turbulence measurements of separate flow nozzles with mixing enhancement features, AIAA-2002-2484
Callender B, Gutmark E, DiMicco R (2002) Design and validation of a coaxial nozzle acoustic test facility, AIAA-2002-0369
Callender B, Gutmark E, Martens S (2004) Far-field acoustic investigation into chevron nozzle mechanisms and trends. AIAA J 43(1):87–95
Callender B, Gutmark E, Martens S (2008) A near-field investigation of chevron nozzle mechanisms. AIAA J 46(1):36–45
Gliebe PR, Brausch JF, Majjigi RK, Lee R (1994) Jet noise suppression. In: Hubbard HH (ed) Aeroacoustics of flight vehicles, vol 2. Acoustical Society of America, New York, pp 207–269
Lu HY (1983) Effect of excitation on coaxial jet noise. AIAA J 21(2):214–220
Peterson RA, Sarohia V (1984) The effect of forward flight on the noise and flow field of inverted profile jets. J Sound Vib 93(1):39–55
Saiyed NH, Bridges JE (1999) Tabs and mixers for reducing low bypass ratio jet noise, AIAA-99-1986
Saiyed NH, Mikkelsen KL, Bridges JE (2000) acoustics and thrust of separate-flow exhaust nozzles with mixing devices for high-bypass-ratio engines, AIAA 2000-1961
Salikuddin M, Martens S, Janardan BA, Shin H, Majjigi RK (1999) Experimental study for multi-lobed mixer high bypass exhaust systems for subsonic jet noise reduction—part 2: acoustic results, AIAA-99-1988
Samimy M, Zaman KBMQ, Reeder MF (1993) Effect of tabs on the flow and noise field of an axisymmetric jet. AIAA J 31(4):609–619
Tam CKW, Zaman KBMQ (2000) Subsonic jet noise from nonaxisymmetric and tabbed nozzles. AIAA J 38(4):592–599
Viswanathan K (2003) Jet aeroacoustic testing: issues and implications. AIAA J 41(9):1674–1689
Acknowledgments
We wish to acknowledge GE Aircraft Engines of Cincinnati, OH, for providing funding and technical assistance with this research study.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Callender, B., Gutmark, E.J. & Martens, S. Flow field characterization of coaxial conical and serrated (chevron) nozzles. Exp Fluids 48, 637–649 (2010). https://doi.org/10.1007/s00348-009-0751-1
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00348-009-0751-1