18th Aerospace Sciences Meeting 1980
DOI: 10.2514/6.1980-54
|View full text |Cite
|
Sign up to set email alerts
|

A multi-stage axial flow compressor mathematical modeling technique with application to two current turbofan compression systems

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

1982
1982
2013
2013

Publication Types

Select...
2
2

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(2 citation statements)
references
References 0 publications
0
2
0
Order By: Relevance
“…The present characteristics h a s been constructed on the few data given in several literature, for example, Chamblebee, Davies, Jr., and Kimzey [11], Davies, Jr. and O'Brien [12], Gamache and Greitzer [13], Greitzer [3], etc. in addition to the existing data.…”
Section: Compressors For the Analysesmentioning
confidence: 99%
“…The present characteristics h a s been constructed on the few data given in several literature, for example, Chamblebee, Davies, Jr., and Kimzey [11], Davies, Jr. and O'Brien [12], Gamache and Greitzer [13], Greitzer [3], etc. in addition to the existing data.…”
Section: Compressors For the Analysesmentioning
confidence: 99%
“…These models have been applied to a variety of compression systems by Kimzey(l) and Chamblee, Davis and Kimzey (2). They are used to analyze and extrapolate the experimental data and to study the effects of unsteady disturbances on the aerodynamic stability of the compression system.…”
Section: Aedc-tr-82-16mentioning
confidence: 99%