Numerical investigation of subsonic flow over bodies of revolution and a typical missile forebody
It was the objective of this investigation to study the subsonic flow over a missile forebody. To this end, the NASA Ames developed OVERFLOW, three dimensional, Navier-Stokes Code was applied and detailed results were obtained for the missile forebody. The flow conditions were set at a Mach Number o...
Main Author: | |
---|---|
Other Authors: | |
Language: | en_US |
Published: |
Monterey, California. Naval Postgraduate School
2013
|
Online Access: | http://hdl.handle.net/10945/35166 |