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Design of a Low Aspect Ratio Transonic Compressor Stage Using CFD Techniques

Design of a Low Aspect Ratio Transonic Compressor Stage Using CFD Techniques PDF Author:
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Languages : en
Pages : 22

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Design of a Low Aspect Ratio Transonic Compressor Stage Using CFD Techniques

Design of a Low Aspect Ratio Transonic Compressor Stage Using CFD Techniques PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

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Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ration of 1.82

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ration of 1.82 PDF Author: Lonnie Reid
Publisher:
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Category : Compressors
Languages : en
Pages : 110

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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Category : Aeronautics
Languages : en
Pages : 702

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Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26 Respectively, and with Design Pressure Ratio of 2.05

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26 Respectively, and with Design Pressure Ratio of 2.05 PDF Author: Royce D. Moore
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Category :
Languages : en
Pages : 108

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Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05 PDF Author: Royce D. Moore
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 120

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Book Description

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 1.82

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 1.82 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 108

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Book Description

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.78, Respectively, and with Design Pressure Ratio of 1.82

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.78, Respectively, and with Design Pressure Ratio of 1.82 PDF Author: Royce D. Moore
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 120

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Time Resolved Measurements in a Low Aspect Ratio Transonic Compressor Stage

Time Resolved Measurements in a Low Aspect Ratio Transonic Compressor Stage PDF Author: A. H. Epstein
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Category :
Languages : en
Pages : 0

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Book Description

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 2.05

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 2.05 PDF Author: Royce D. Moore
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 108

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Book Description

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and with Design Pressure Ratio of 2.05 PDF Author: Royce D. Moore
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 120

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Book Description