Design of Curved Annular Diffusers

Author:

Kuchana Vinayender1,Balakrishnan N.2,Srinivasan Balamurugan3

Affiliation:

1. Technology Specialist, Honeywell 500019, Hyderabad, India

2. Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560012, India

3. Honeywell 560103, Bengaluru, India

Abstract

Abstract Influence of curvature distribution and area-ratio (AR) distribution on the pressure fields within the curved annular diffuser are discussed. General guidelines for end-wall contouring to control the pressure gradients on the diffuser walls are evolved and further demonstrated through computational fluid dynamics (CFD) simulations. Also, detailed guidelines for controlling the adverse pressure gradients (APG) on duct walls are presented. A geometry generation methodology (GGM) which enables both design and evaluation of curved annular diffusers based on the guidelines evolved is presented. The approach presented deals with the sensitivity of the duct performance parameters to duct wall modifications. In that sense, the work per se is not a description of an automated optimization process, but rather about the physical principles that can guide such an optimization. An aggressive diffuser design space is identified with ducts of maximum slope of 50 deg and maximum divergence angle between the outer and inner walls of 10 deg for length to inlet height ratio ranging from 1.25 to 2.5. Part of the identified design space for which the flow separation can be eliminated based on the guidelines evolved is demarcated. The need for flow control, possibly passive, is established for more aggressive designs.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference20 articles.

1. Research on the Aerodynamics of Intermediate Turbine Diffusers;Elsevier, Prog. Aerosp. Sci.,2011

2. The Influence of Blade Wakes on the Performance of Inter-Turbine Diffusers;ASME J. Turbomach.,1996

3. Flow Development Through Inter-Turbine Diffusers;ASME J. Turbomach.,1998

4. Flow and Loss Mechanisms Within an Interturbine Duct;AIAA. J. Propul. Power,2016

5. Numerical Investigation of the Effect of Tip Leakage Flow on an Aggressive S-Shaped Intermediate Turbine Duct

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1. Design of Curved Annular Diffusers II: Using Splitter Blades;Journal of Engineering for Gas Turbines and Power;2022-06-02

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