Characterization of the Flowfield near a Wrap-Around Fin at Mach 2.8

The Navier-Stokes equations have been solved in the vicinity of a single wrap-around fin mounted on a semicylindrical missile body shape with the objective of quantifying the flow structure in the region near the fin/body juncture (Mach number 2.8, unit Reynolds number 18 x 10 6 m -1). The Baldwin-...

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Veröffentlicht in:	Journal of aircraft 1998-11, Vol.35 (6), p.868-875
Hauptverfasser:	Tilmann, C. P, Buter, T. A, Bowersox, R. D. W
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics Design Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical models Missiles Physics Velocity
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Zusammenfassung:	The Navier-Stokes equations have been solved in the vicinity of a single wrap-around fin mounted on a semicylindrical missile body shape with the objective of quantifying the flow structure in the region near the fin/body juncture (Mach number 2.8, unit Reynolds number 18 x 10 6 m -1). The Baldwin- Lomax algebraic eddy viscosity model was employed.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/2.2406