Supersonic nozzle design of arbitrary cross-section
An investigation, both theoretical and experimental in nature, has been undertaken to develop a simple method for the design of supersonic nozzles and, indeed, inlets of quite complex shapes from known or calculated axisymmetric flowfields. 1he axisymmetric flowfield is determined using a computer p...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en |
| Published: |
Cranfield University
2009
|
| Online Access: | http://hdl.handle.net/1826/3512 |