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Journal ArticleDOI

CFD-Based Three-Dimensional Turbofan Exhaust Nozzle Analysis System

B. D. Keith, +2 more
- 01 Nov 1993 - 
- Vol. 9, Iss: 6, pp 840-846
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TLDR
In this paper, a three-dimensional turbofan exhaust nozzle analysis system based on computational fluid dynamics (CFD) has been developed to aid exhaust designers in the efficient assessment and screening of their design concepts, with the prospects of a reduction in both design cycle time and wind-tunnel test costs.
Abstract
A three-dimensional turbofan exhaust nozzle analysis system based on computational fluid dynamics (CFD) has been developed. This system has been established to aid exhaust designers in the efficient assessment and screening of their design concepts, with the prospects of a reduction in both design cycle time and wind-tunnel test costs. A reliable CFD flow solver, user-friendly grid generator, and postprocessing software are included in the system. The system is easy to use for exhaust designers who are not particularly familiar with the inner workings of CFD. Validation and applicability studies have been performed using different exhaust nozzle configurations at on-design and off-design engine operating conditions. This work demonstrates that a CFD code integrated with automatic grid generation and postprocessing can be a useful analytical tool in the practical exhaust nozzle design process. Nomenclature M = Mach number P = static pressure PA = atmospheric static pressure R = radius X — axial station XREF = reference length Subscript 00 = freestream conditions

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Citations
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Journal ArticleDOI

Civil turbofan engine exhaust aerodynamics: impact of bypass nozzle after-body design

TL;DR: In this paper, a parametric geometry definition has been derived based on Class-Shape Transformation (CST) functions for the representation of post-nozzle-exit components such as after-bodies, plugs, and air-flow vents.
Journal ArticleDOI

Commercial turbofan engine exhaust nozzle flow analyses

TL;DR: In this paper, a three-dimensional code is developed for solving the simplified Reynolds-averaged NavierStokes equations in a 3D multiblock/mul tizone structured mesh domain.

Combined Numerical/Analytical Perturbation Solutions of the Navier-Stokes Equations for Aerodynamic (Ejector Nozzle) Flows

TL;DR: Differential Reduced Ejector/Mixer Analysis (DREA) as discussed by the authors is a combined perturbation/numerical modeling methodology with an application to ejector-mixer nozzles.
Journal ArticleDOI

Civil turbofan engine exhaust aerodynamics: Impact of fan exit flow characteristics

TL;DR: In this article, a combined design space exploration (DSE) and exhaust geometry optimization is performed to optimize the exhaust geometry in conjunction with the fan exit profile to achieve significant performance improvement compared to the fixed inflow cases.
Journal ArticleDOI

Aerodynamic design of an ultra-low rotating speed geared fan

TL;DR: In this paper, the authors presented a diffusion blade profiles for designing a fan rotor with an ultra-low rotating speed, which is characterized by large cambers and convergent blade passages in their rear parts.
References
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Journal ArticleDOI

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