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.
| Author | : Albert L. Johns |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1969 |
| Genre | : |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 962 |
| Release | : 1970 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 956 |
| Release | : 1970 |
| Genre | : Science |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 784 |
| Release | : 1969-10 |
| Genre | : Science |
| ISBN | : |
| Author | : Douglas E. Harrington |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1974 |
| Genre | : Jet nozzles |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 702 |
| Release | : 1976 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Douglas E. Harrington |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1976 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : Douglas E. Harrington |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1974 |
| Genre | : Airplanes |
| ISBN | : |
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 | : |
| Total Pages | : 60 |
| Release | : 1970 |
| Genre | : |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 966 |
| Release | : 1970 |
| Genre | : Aeronautics |
| ISBN | : |
