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Annular truncated plug nozzle flowfield and base pressure characteristics.The flowfield and base pressure characteristics of an internal-external expansion, truncated plug nozzle are described over the pressure ratio range from 'open' wake to 'closed' wake conditions. The effect of plug length on these characteristics, including the process of wake 'closure' is also presented. An existing method for calculating the flowfield and base pressure, for 'closed' wake operation, is modified to include the internal shock wave generated near the shroud exit. The supersonic portion of the flow is calculated using rotational axisymmetric method of characteristics. The technique of Hartree is employed so that the downstream characteristic point locations can be chosen to fit the developing flowfield. An overexpansion technique is used to detect the internal shock wave in the vicinity of the shroud exit so that its effect on the plug base pressure could be determined. Good agreement between the analytical results and experimental data is obtained for 'closed' wake operations.
Document ID
19730032085
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sule, W. P.
Mueller, T. J.
(Notre Dame, University Notre Dame, Ind., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 73-137
Report Number: AIAA PAPER 73-137
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 10, 1973
End Date: January 12, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A16887
Funding Number(s)
CONTRACT_GRANT: NAS8-25601
Distribution Limits
Public
Copyright
Other

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