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Experimental and computational analysis of a tangent ogive slender body at incompressible speeds (2017)
Journal Article
Schoombie, J., Tuling, S., & Dala, L. (2017). Experimental and computational analysis of a tangent ogive slender body at incompressible speeds. Aerospace Science and Technology, 69, 474-484. https://doi.org/10.1016/j.ast.2017.06.011

© 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
Tuling, S., Vallabh, B., & Morelli, M. F. (2015). Compressibility effects for the AGARD-B model. Aeronautical Journal, 119(1214), 543-552. https://doi.org/10.1017/S0001924000010605

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 be... Read More about Compressibility effects for the AGARD-B model.

Two-dimensional potential method simulations of a body-strake configuration (2014)
Journal Article
Toomer, C., Tuling, S., Dala, L., & Toomer, C. (2014). Two-dimensional potential method simulations of a body-strake configuration. Journal of Spacecraft and Rockets, 51(2), 468-477. https://doi.org/10.2514/1.A32565

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.

Some compressibility effects on the lee side flow structures of cruciform wing–body configurations with very low aspect ratio wings (2013)
Journal Article
Tuling, S., Dala, L., & Toomer, C. (2013). Some compressibility effects on the lee side flow structures of cruciform wing–body configurations with very low aspect ratio wings. Aerospace Science and Technology, 29(1), 373-385. https://doi.org/10.1016/j.ast.2013.04.008

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 flo... Read More about Some compressibility effects on the lee side flow structures of cruciform wing–body configurations with very low aspect ratio wings.


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