An Experimental Two-stage Transonic Compressor

An Experimental Two-stage Transonic Compressor PDF Author: G. E. Jeffery
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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An Experimental Two-stage Transonic Compressor

An Experimental Two-stage Transonic Compressor PDF Author: G. E. Jeffery
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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Book Description


An Experimental Two-stage Transonic Compressor

An Experimental Two-stage Transonic Compressor PDF Author: R. K. Oldham
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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An Experimental Two-stage Transonic Compressor

An Experimental Two-stage Transonic Compressor PDF Author: D. C. Dransfield
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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An Experimental Two-stage Transonic Compressor

An Experimental Two-stage Transonic Compressor PDF Author: M. G. Philpot
Publisher:
ISBN:
Category :
Languages : en
Pages : 27

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Dynamic Inlet Distortion Experiments on a Two-stage Transonic Compressor

Dynamic Inlet Distortion Experiments on a Two-stage Transonic Compressor PDF Author: R. K. Oldham
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860

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The Aerothermodynamics of Aircraft Gas Turbine Engines

The Aerothermodynamics of Aircraft Gas Turbine Engines PDF Author:
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 770

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494

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Comparison of Experimentally and Analytically Determined Windmilling Characteristics of a Compressor with Low Over-all Pressure Ratio

Comparison of Experimentally and Analytically Determined Windmilling Characteristics of a Compressor with Low Over-all Pressure Ratio PDF Author: James E. Hatch
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 20

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Book Description
Windmilling tests on a two-stage transonic compressor with a design over-all pressure ratio of 1.85 produced the following results. The maximum windmilling equivalent speed was 30.2 percent of design speed, and the maximum windmilling equivalent flow was 57.4 percent of the design flow. The maximum flow was limited by choking in the last stator passage. A method was developed for estimating maximum windmilling speed and flow from known compressor design values and geometry for a compressor with exit stators. The method, which is based on the results of the analysis of the windmilling data, predicts the maximum windmilling equivalent speed within 3.3 percent and the maximum windmilling equivalent flow within 0.4 percent.