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

Jayaraman, V (1987) Wind tunnel testing on underwater axisymmetric bodies at angle of attack Part III - Experimental investigation on an axisymmetric Body with Blunt Nose. Project Report. National Aerospace Laboratories, Bangalore.

[img] PDF
PD_FM_8708.pdf
Download (94kB)

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.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Wind tunnel testing;Surface pressure measurement;Blunt nose
Subjects: AERONAUTICS > Aerodynamics
ENGINEERING > Fluid Mechanics and Thermodynamics
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 25 Jul 2012 06:22
Last Modified: 25 Jul 2012 06:22
URI: http://nal-ir.nal.res.in/id/eprint/10649

Actions (login required)

View Item View Item
nalir is powered by EPrints 3 which is developed by the School of Electronics and Computer Science at the University of Southampton. More information and software credits.