Preliminary design code for an axial stage compressor
Current two-dimensional preliminary design codes use structured programming, which is rigid and does not allow the user to vary parameters easily. This study uses object-oriented programming to allow the user to vary all selectable parameters in a familiar Windows operating environment. The programm...
Main Author: | Ramakdawala, Rizwan R. |
---|---|
Other Authors: | Shreeve, Raymond P. |
Format: | Others |
Published: |
Monterey, California. Naval Postgraduate School
2012
|
Online Access: | http://hdl.handle.net/10945/1494 |
Similar Items
-
Preliminary aerothermal design of axial compressors
by: Piscopo, Giovanni
Published: (2013) -
TO THE OPTIMUM DESIGN OF THE AXIAL MULTI-STAGE COMPRESSOR
by: Владимир Петрович Герасименко, et al.
Published: (2017-08-01) -
Design and analysis of axial aspirated compressor stages
by: Merchant, Ali A. (Ali Abbas)
Published: (2005) -
Unsteadiness In An Embedded Axial Compressor Stage
by: Naylor, Edward
Published: (2011) -
Unsteadiness in an embedded axial compressor stage
by: Naylor, Edward
Published: (2008)