Investigation of the Performance of a Turbojet Engine with Variable-position Compressor Inlet Guide Vanes PDF Download
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Author: Ray E. Budinger
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
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Book Description
Author: Ray E. Budinger
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
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Author: S.C. Huntley
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Author: Carl E. Campbell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
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Book Description
Compressor performance and turbine performance are presented in the form of performance maps at selected values of Reynolds number index; the effects of Reynolds number on performance are summarized. The effects of variable stator angle and high inlet-air temperatures on compressor performance are also shown. Over-all engine performance (net thrust and specific fuel consumption) is presented for a flight Mach number of 0.9 at rated engine conditions over a range of altitudes to illustrate performance losses resulting from decreased Reynolds number index.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Book Description
Author: David N. Bowditch
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
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Author: W.F. Dobson
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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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:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
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