NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Cylindrical diffuser performance using a truncated plug nozzleCylindrical diffuser performance for a truncated plug nozzle without external flow was tested in a blowdown wind tunnel. The nozzle was designed for an exit Mach number of 1.9 and the plug was conical in shape from the throat and converged to the axis of symmetry at an angle of 10 degrees. The diffuser section was fashioned into two 13.97 cm lengths to facilitate boring of the duct diameter and to allow for testing of two different duct lengths. A slotted hypotube was installed in the base of the diffuser to measure pressure distribution down the centerline of the diffuser. The data obtained included: the typical centerline and sidewall pressure ratio variation along the diffuser, cell pressure ratio vs overall pressure ratio for long and short diffusers and a comparison of minimum experimental cell pressure ratio vs area ratio.
Document ID
19760050025
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Galanga, F. L.
(Notre Dame Univ. IN, United States)
Mueller, T. J.
(Notre Dame, University Notre Dame, Ind., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1976
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 13
Subject Category
Aerodynamics
Accession Number
76A32991
Funding Number(s)
CONTRACT_GRANT: NAS8-25601
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available