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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Citation Formats

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.