28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-2.8.3
AN EXPERIMENTAL AND NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT TRANSONIC SPEED
S. A. Prince, N. G. Goizueta
City Univ., London, UK
Keywords: experimental, computational, nose blunting, transonic speed
An experimental and computational study on the aerodynamic effect of nose blunting on a conical nosed slender axisymmetric body was studied. Data is presented across the Mach number range 0.1 – 5.0, and for angle of incidence 0 deg - 15 deg for transonic cases.
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