Experimental Investigation of Acceleration Characteristics of a Turbojet Engine Including Regions of Surge and Stall for Control Applications PDF Download
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Author: Paul M. Stiglic
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Author: Paul M. Stiglic
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Author: Frank L. Oppenheimer
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ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 494
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Author: Ross D. Schmidt
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ISBN:
Category : Aeronautics
Languages : en
Pages : 38
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During the course of an investigation of an axial-flow turbojet engine in the Lewis altitude wind tunnel, limitations on the transient operation of the engine were determined to relation to two altitudes and exhaust-nozzle-areas. Below approximately 70 percent of the generalized engine rotational speed, a high-frequency oscillation (stall) at the compressor inlet limited transient operation of the engine. Over 70 percent of the engine speed, transient operation was limited by a low-frequency oscillation (surge), which occurred throughout the engine.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1812
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 624
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