Passive devices for axisymmetric base drag reduction at transonic speeds
R. Viswanath
Abstract
R. Viswanath
Abstract
Experiments have been made to assess the effectiveness of several base modifications or passive devices for reducing base drag and total afterbody drag at transonic speeds. The modifications tested include base cavities, ventilated cavities, and two vortex suppression devices. Results show that, while appreciable base drag reductions are possible with many of the devices examined, the net total drag reductions are relatively lower, presumably because of the additional losses associated with the devices. (Author)
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Experiments have been made to assess the effectiveness of several base modifications or passive devices for reducing base drag and total afterbody drag at transonic speeds. The modifications tested include base cavities, ventilated cavities, and two vortex suppression devices. Results show that, while appreciable base drag reductions are possible with many of the devices examined, the net total drag reductions are relatively lower, presumably because of the additional losses associated with the devices. (Author)
Key concepts: Transonic, Drag, Reduction (mathematics), Drag divergence Mach number, Aerospace engineering, Rotational symmetry, Lift-induced drag, Lift-to-drag ratio