Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source
Author: Albert L. Johns
Publisher:
Published: 1969
Total Pages: 38
ISBN-13:
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Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source
Author: Albert L. Johns
Publisher:
Published: 1969
Total Pages: 40
ISBN-13:
DOWNLOAD EBOOKNASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published: 1970
Total Pages: 966
ISBN-13:
DOWNLOAD EBOOKA Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Published: 1970
Total Pages: 962
ISBN-13:
DOWNLOAD EBOOKNASA 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:
Published: 1970
Total Pages: 956
ISBN-13:
DOWNLOAD EBOOKCold-flow Performance of Several Variations of a Ram-air-cooled Plug Nozzle for Supersonic-cruise Aircraft
Author: Douglas E. Harrington
Publisher:
Published: 1974
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKThrust 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:
Published: 1976
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKThrust 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:
Published: 1974
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKPlug 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:
Published: 1970
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKThrust 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:
Published: 1975
Total Pages: 52
ISBN-13:
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