Author: Tsuguji Nakano
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical and Experimental Investigation of Instability Inception in a High-speed Axial-flow Compressor Using Chaos Theory
Author: Tsuguji Nakano
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-4050 - 02-4099
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
Compressor Instability with Integral Methods
Author: Eddie Y.K. Ng
Publisher: Springer Science & Business Media
ISBN: 3540724125
Category : Technology & Engineering
Languages : en
Pages : 154
Book Description
This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also serve as self-study material.
Publisher: Springer Science & Business Media
ISBN: 3540724125
Category : Technology & Engineering
Languages : en
Pages : 154
Book Description
This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also serve as self-study material.
Analysis of Instability Inception in High-speed Multi-stage Axial-flow Compressors
Author: Gavin J. Hendricks
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996.
Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss
Author: Kenneth Lee Suder
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 272
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 272
Book Description
Investigation of an Impulse Axial-flow Compressor
Author: John R. Erwin
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 56
Book Description
Design and Tests of a Six-stage Axial-flow Compressor Having a Tip Speed of 550 Feet Per Second and a Flat Operating Characteristic at Constant Speed
Author: Willard R. Westphal
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 66
Book Description
A six-stage axial-flow compressor with a tip speed of 550 feet per second and a flat operating characteristics at constant speed has been designed and tested. It was designed for a constant power input per pound of flow in expectation that this would result in a wider mass-flow operating range at a given stagnation-presssure ratio. The design specific weight flow was 21.3 pounds per second per square foot of frontal area at atmospheric discharge with a stagnation-pressure ratio of 3.25 and an inlet hub-tip radius ratio of 0.7. Several configurations consisting of various blade setting angles and solidities were tested. Tests showed that the design flow, pressure ratio, and flat operating characteristic were obtained over a range of 10 percent of design flow at a peak efficiency of 82 percent for design conditions. The compressor had a possible immediate application for air removal from a large slotted-throat transonic wind tunnel, but the design theory could apply to any low-speed industrial compressor or second spool of a turbojet engine.
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 66
Book Description
A six-stage axial-flow compressor with a tip speed of 550 feet per second and a flat operating characteristics at constant speed has been designed and tested. It was designed for a constant power input per pound of flow in expectation that this would result in a wider mass-flow operating range at a given stagnation-presssure ratio. The design specific weight flow was 21.3 pounds per second per square foot of frontal area at atmospheric discharge with a stagnation-pressure ratio of 3.25 and an inlet hub-tip radius ratio of 0.7. Several configurations consisting of various blade setting angles and solidities were tested. Tests showed that the design flow, pressure ratio, and flat operating characteristic were obtained over a range of 10 percent of design flow at a peak efficiency of 82 percent for design conditions. The compressor had a possible immediate application for air removal from a large slotted-throat transonic wind tunnel, but the design theory could apply to any low-speed industrial compressor or second spool of a turbojet engine.
Numerical and Experimental Investigations of Unsteady Flows in Low-speed Axial Compressors
Author: M. A. Langley
Publisher:
ISBN:
Category :
Languages : en
Pages : 265
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 265
Book Description
Aerodynamic Design of Axial-flow Compressors
Author: Lewis Research Center
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 542
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 542
Book Description
An Investigation of the Surge Behavior of a High-speed Ten-stage Axial Flow Compressor
Author: Patrick M. Russler
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 330
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 330
Book Description