Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons

8Citations
Citations of this article
15Readers
Mendeley users who have this article in their library.

Abstract

Variation of the bypass nozzle exit area enables optimization of the turbofan engine operating cycle over a wider range of operational conditions resulting in improved thrust and/or fuel consumption. Two mechanisms for varying the nozzle area have been investigated. The first uses an array of chevrons which when closed, form a full body of revolution and when warped/curved, increase the exit area while forming a serrated trailing edge. The second technique incorporates an axially translating section of the nacelle shroud and uses the change in the nozzle boat-tail radial location with the axial location as a means to vary the nozzle exit area. To analyse the effects on a typical rotor/stator stage, computational fluid dynamics simulations of the NASA Rotor 67, Stator 67A stage integrated into a custom-built nacelle were performed. Nozzles with 8, 12, and 16 chevrons were simulated to evaluate the impact of the variation in geometry upon the nacelle wake and local forces. Gross thrust of the nacelle and the turbulent kinetic energy (TKE) variation through the wake is compared. The chevron nozzle attains a nearly 2 per cent maximum thrust improvement over the translating nozzle technique. The chevron nozzle also has significantly lower (nearly 8 per cent) peak TKE levels in the jet plume.

Cite

CITATION STYLE

APA

Sloan, B., Wang, J., Spence, S., Raghunathan, S., & Riordan, D. (2010). Aerodynamic performance of a bypass engine with fan nozzle exit area change by warped chevrons. In Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering (Vol. 224, pp. 731–743). https://doi.org/10.1243/09544100JAERO529

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free