Author: G. E. Jeffery
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
An Experimental Two-stage Transonic Compressor
Author: G. E. Jeffery
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
An Experimental Two-stage Transonic Compressor
Author: R. K. Oldham
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
An Experimental Two-stage Transonic Compressor
Author: D. C. Dransfield
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
An Experimental Two-stage Transonic Compressor
Author: M. G. Philpot
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Dynamic Inlet Distortion Experiments on a Two-stage Transonic Compressor
Author: R. K. Oldham
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
The Aerothermodynamics of Aircraft Gas Turbine Engines
Author:
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 770
Book Description
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 770
Book Description
Index of NASA Technical Publications
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
Book Description
Comparison of Experimentally and Analytically Determined Windmilling Characteristics of a Compressor with Low Over-all Pressure Ratio
Author: James E. Hatch
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 20
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.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 20
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.