Title of article
Analysis on numerical results for stage separation with different exhaust holes
Author/Authors
Tzong-Hann Shieh، نويسنده , , Tong-Miin Liou، نويسنده , , Meng-Rong Li، نويسنده , , Cheng-Hsin Liu، نويسنده , , Wen-Jing Wu، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2009
Pages
4
From page
342
To page
345
Abstract
The flow field for thermal stage separation is carried out and predicted by unsteady numerical simulation with the dynamic moving grids in this work. The overset grids are applied to simulate the relative separating motion of multi-stage rocket. The flow problems and effects of different exhaust holes within the interstage under considering the design of thermal stage separation are systematically computed, discussed and also analyzed.
Keywords
Thermal stage separation , Over-expanded nozzle , Navier–Stokes equations , Overset grids , Interstage
Journal title
International Communications in Heat and Mass Transfer
Serial Year
2009
Journal title
International Communications in Heat and Mass Transfer
Record number
1220480
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