Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor PDF Download
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Author: Kenneth Lee Suder
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Author: Kenneth Lee Suder
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Author: Chetan S. Mistry
Publisher: Springer Nature
ISBN: 9811550395
Category : Technology & Engineering
Languages : en
Pages : 534
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Book Description
This volume presents selected papers presented during the National Aerospace Propulsion Conference (NAPC) held at Indian Institute of Technology Kharagpur. It brings together contributions from the entire propulsion community, spanning air-breathing and non-air-breathing propulsion. The papers cover aerospace propulsion-related topics, and discuss relevant research advances made in this field. It will be of interest to researchers in industry and academia working on gas turbine, rocket, and jet engines.
Author: Kenneth Lee Suder
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 272
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 630
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 410
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Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 498
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Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 436
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Author: Kenneth L. Suder
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2 - Jun 5, 1997.
Author: Rodrick V. Chima
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
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Book Description
The flow through the tip clearance region of a transonic compressor rotor (NASA rotor 37) was computed and compared to aerodynamic probe and laser anemometer data. Tip clearance effects were modeled both by gridding the clearance gap and by using a simple periodicity model across the ungridded gap. The simple model was run with both the full gap height, and with half the gap height to simulate a vena-contracta effect. Comparisons between computed and measured performance maps and downstream profiles were used to validate the models and to assess the effects of gap height on the simple clearance model. Recommendations were made concerning the use of the simple clearance model. Detailed comparisons were made between the gridded clearance gap solution and the laser anemometer data near the tip at two operating points. The computer results agreed fairly well with the data but overpredicted the extent of the casing separation and underpredicted the wake decay rate. The computations were then used to describe the interaction of the tip vortex, the passage shock, and the casing boundary layer.
