Calculation of Symmetric and Asymmetric Vortex Seperation on Cones and Tangent Ogives Based on Discrete Vortex Models

By: Nasa, National Aeronautics and Space Adm

An inviscid discrete vortex model, with newly derived expressions for the tangential velocity imposed at the separation points, is used to investigate the symmetric and asymmetric vortex separation on cones and tangent ogives. The circumferential locations of separation are taken from experimental data. Based on a slender body theory, the resulting simultaneous nonlinear algebraic equations in a cross-flow plane are solved with Broyden's modified Newton-Raphson method. Total force coefficients are obtained through momentum principle with new expressions for nonconical flow. It is shown through the method of function deflation that multiple solutions exist at large enough angles of attack, even with symmetric separation points. These additional solutions are asymmetric in vortex separation and produce side force coefficients which agree well with data for cones and tangent ogives. Chin, S. and Lan, C. Edward Unspecified Center...

• Format: Paperback
• Language: English
• ISBN: 1730931251
• ISBN13: 9781730931253
• Release Date: January 1
• Publisher: Independently Published
• Length: 94 Pages
• Weight: 0.53 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"