Sean Tuling's Outputs (5)

Experimental and computational analysis of a tangent ogive slender body at incompressible speeds (2017)
Journal Article

© 2017 Elsevier Masson SAS A combined computational and experimental analysis was performed on a tangent ogive body with very low aspect ratio wings in the ‘+’ (plus) orientation at Mach numbers 0.1, 0.2 and 0.3, with the aim of developing a database... Read More about Experimental and computational analysis of a tangent ogive slender body at incompressible speeds.

Compressibility effects for the AGARD-B model (2015)
Journal Article

A numerical study of the flow topologies over the 60° delta wing of the AGARD-B model at Mach 0 · 80 has revealed that vortex bursting occurs between 13°-15° angle-of-attack, while vortex separation occurs above 18°. These aerodynamic features have b... Read More about Compressibility effects for the AGARD-B model.

Two-dimensional potential method simulations of a body-strake configuration (2014)
Journal Article

The lee-side flow over a cruciform wing-body configuration at supersonic speeds in the "+" orientation up to angles of 25 deg have been simulated using the single concentrated vortex and discrete vortex model methods. The wings or strakes are of very... Read More about Two-dimensional potential method simulations of a body-strake configuration.

Lee-side flow structures of very low aspect ratio cruciform wing–body configurations (2013)
Journal Article

Anumerical and experimental investigation was performed to study the dominant flow structures in the lee side of a cruciform wing-body configuration at supersonic speeds in the + orientation. The wings or strakes are of very low aspect ratio of order... Read More about Lee-side flow structures of very low aspect ratio cruciform wing–body configurations.

Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings (2013)
Journal Article

A series of validated numerical simulations of a tangent ogive circular body in combination with very low aspect ratio cruciform wings at supersonic Mach numbers and angles of attack up 25 have been performed. Inspection of the flow in the cross flow... Read More about Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings.