Performance Characteristics of a 10 Deg Conical Plug Nozzle at Mach Numbers Up to 1 29
Author:
Publisher:
Published: 1964
Total Pages: 54
ISBN-13:
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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 EBOOKPerformance of a 10 Deg Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0
Author: Fred W. Steffen
Publisher:
Published: 1970
Total Pages: 36
ISBN-13:
DOWNLOAD EBOOKExperimental Investigation of a 10 Deg Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0
Author: Donald L. Bresnahan
Publisher:
Published: 1969
Total Pages: 46
ISBN-13:
DOWNLOAD EBOOKPerformance of a 10 Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0
Author: Fred W. Steffen
Publisher:
Published: 1970
Total Pages: 26
ISBN-13:
DOWNLOAD EBOOKPerformance of Convergent and Plug Nozzles at Mach Numbers from 0 to 1.97
Author: Douglas E. Harrington
Publisher:
Published: 1970
Total Pages: 46
ISBN-13:
DOWNLOAD EBOOKScientific and Technical Aerospace Reports
Author:
Publisher:
Published: 1987
Total Pages: 1126
ISBN-13:
DOWNLOAD EBOOKLists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Coolant Flow Effects on the Performance of a Conical Plug Nozzle at Mach Numbers from 0 to 2.0
Author: Robert J. Jeracki
Publisher:
Published: 1970
Total Pages: 60
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 EBOOKExperimental Investigation of a 10 Conical Turbojet Plug Nozzle with IRIS Primary and Translating Shroud at Mach Numbers from 0 to 2.0
Author: Donald L. Bresnahan
Publisher:
Published: 1968
Total Pages: 41
ISBN-13:
DOWNLOAD EBOOKAn experimental investigation was conducted in the Lewis Research Center's nozzle static test facility and the 8 by 6 foot supersonic wind tunnel to determine the performance characteristics of a 10 half-angle conical turbojet plug nozzle wih a simutated iris primary throat and overall design pressure ratio of 26.3.
