Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source PDF full book. Access full book title Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source by Albert L. Johns. Download full books in PDF and EPUB format.
Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Get Book Here
Book Description
Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Get Book Here
Book Description
Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Get Book Here
Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
Get Book Here
Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Get Book Here
Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Get Book Here
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
Get Book Here
Book Description
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Get Book Here
Book Description
