Design of Curved Annular Diffusers II: Using Splitter Blades

Author:

Kuchana Vinayender1,Balakrishnan N.2,Srinivasan Balamurugan3

Affiliation:

1. Honeywell , Hyderabad 500019, India

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

3. Honeywell , Bengaluru 560103, India

Abstract

Abstract The use of splitter blade as a passive flow control mechanism in the design of separation free aggressive annular diffuser is explored through computational fluid dynamics simulations. The fundamental working principle of a splitter blade in case of a two-dimensional rectangular diffuser and an annular diffuser is discussed. The effects of splitter blade configuration on the end-wall adverse pressure gradients are discussed. 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 axial-length to inlet height ratio ranging from 1.25 to 2.5. One or more splitter blades are employed in the duct to eliminate flow separation for all the ducts in the aggressive design space considered. Requirement of number of splitter blades in the aggressive design space is demarcated. Performance charts for the ducts in this aggressive design space are also established.

Publisher

ASME International

Subject

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

Reference26 articles.

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

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

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

4. Numerical Investigation of the Effect of Tip Leakage Flow on an Aggressive S-Shaped Intermediate Turbine Duct,2009

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