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Potential flow solutions with wakes over an ogive cylinder
Date
1998-05-01
Author
Tuncer, İsmail Hakkı
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An incompressible panel code is employed to compute the flow over an ogive cylinder body with an overall length of 7.5 diameter. Flow separation is modeled by vortex wakes attached to the base region and the leeward sides of the cylinder body. The computed surface pressures and integrated normal force and pitching-moment coefficients are found to be in good agreement with the experimental data up to 20-deg incidence. This favorable agreement suggests that the panel codes may be a computationally efficient tool in the aerodynamic missile design process at low incidences.
Subject Keywords
Space and Planetary Science
,
Aerospace Engineering
URI
https://hdl.handle.net/11511/57069
Journal
JOURNAL OF SPACECRAFT AND ROCKETS
DOI
https://doi.org/10.2514/2.3351
Collections
Department of Aerospace Engineering, Article
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İ. H. Tuncer, “Potential flow solutions with wakes over an ogive cylinder,”
JOURNAL OF SPACECRAFT AND ROCKETS
, pp. 273–277, 1998, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57069.