Author: Albert L. Johns
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source
Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
Book Description
Cold-flow Performance of Several Variations of a Ram-air-cooled Plug Nozzle for Supersonic-cruise Aircraft
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
Book Description
Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Thrust Performance of Isolated Plug Nozzles with Two Types of 40-spoke Noise Suppressor at Mach Numbers from 0 to 0.45
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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.
Performance of a 10° Conical Plug Nozzle with Various Primary Flap and Nacelle Configurations at Mach Numbers from 0 to 1.97
Author: Douglas E. Harrington
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Thrust Performance of Isolated 36-chute Suppressor Plug Nozzles with and Without Ejectors at Mach Numbers from 0 to 0.45
Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description