Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source PDF Download
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Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Book Description
Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Book Description
Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
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Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
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Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
Plug nozzles with two types of 40-spoke noise suppressor were tested at free-stream Mach numbers from 0 to 0.45 and over a range of nozzle pressure ratios from 1.5 to 4.0. In addition, an unsuppressed plug nozzle and a Supersonic Tunnel Association nozzle were also tested to provide baseline levels of thrust performance. The unsuppressed plug nozzle had an efficiency of 98 percent at an assumed takeoff pressure ratio of 3.0 and at Mach 0.36. At the same condition the suppressor nozzles had efficiencies of approximately 83.5 percent.
Author: Douglas E. Harrington
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
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Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
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Book Description
