Nair, Manoj T and Kumar, Naresh and Saxena, SK (2005) Computational Analysis of Inlet Aerodynamics for a Hypersonic Research Vehicle. Journal of Propulsion and Power, 21 (21). pp. 286-291.
Full text not available from this repository.Abstract
The aim of the present work is to carry out Reynolds-averaged Navier-Stokes computations of flow through the inlet of a hypersonic research vehicle with a view to accomplish detailed aerodynamic analysis. Three inlet configurations that differ in the inlet-duct height are considered in this study. The results of this study are13; presented in the form of detailed computational flow visualization through density contours, variation of flow parameters at various desired sections, and inlet performance in each case.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Hypersonic vehicles;Inlet flow;Reynolds averaged Navier-Stokes method;Ducted flow;Flow visualization;Computational fluid dynamics;Flow characteristics; Aerodynamics;Research vehicles |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 14 Nov 2005 |
| Last Modified: | 24 May 2010 04:09 |
| URI: | http://nal-ir.nal.res.in/id/eprint/843 |
Actions (login required)
 |
View Item |
