NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical and experimental evaluation of a new low-leakage labyrinth sealThe effectiveness of a recently developed leakage model for evaluating new design features of most seals is demonstrated. A preliminary assessment of the present stator groove feature shows that it gives approximately a 20 percent leakage reduction with no shaft speed effects. Also, detailed distributions of predicted streamlines, axial velocity, relative pressure and turbulence energy enhance one's physical insight. In addition, the interesting measured effect of axial position of the rotor/stator pair on leakage rate and stator wall axial pressure distribution is examined.
Document ID
19880063555
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rhode, D. L.
(Texas A&M Univ. College Station, TX, United States)
Ko, S. H.
(Texas A&M Univ. College Station, TX, United States)
Morrison, G. L.
(Texas A & M University College Station, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 88-2884
Accession Number
88A50782
Distribution Limits
Public
Copyright
Other

Available Downloads

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