Wind tunnel testing on underwater axisymmetric bodies at angle of attack Part III - Experimental investigation on an axisymmetric Body with Blunt Nose

Abstract

This report, describes the details of the surface pressure measurements made on an axisymmetric body, of finness ratio 15, having blunt nose. The model was tested in the 0.9m dia Low Speed Tunnel at various incidences. The results are presented in this report in the forms of tables and figures