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.
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:||Journal 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)|
|Division/Department:||Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division|
|Depositing User:||Ms Indrani V|
|Date Deposited:||14 Nov 2005|
|Last Modified:||24 May 2010 09:39|
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