Gasdynamics and Heat Transfer Modeling in Rocket Joints

A new thermal-flow simulation code has been developed to model the gasdynamics and heat transfer, as well as O-ring and flow path erosions inside the Space Shuttle solid rocket motor joints by combining a thermal analyzer and a general-purpose computational fluid dynamics code. The pressure, tempera...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of spacecraft and rockets 2001-09, Vol.38 (5), p.777-788
Hauptverfasser:	Wang, Qunzhen, Mathias, Edward C, Heman, Joe R, Smith, Cory W
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Computational fluid dynamics Friction Heat flux Heat transfer Leakage (fluid) Mathematical models Navier Stokes equations Space shuttles Thermoanalysis
Online-Zugang:	Volltext
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