Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel.

Krishnamurthy, K (1989) Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel. Technical Report. NAL, Bangalore.

[img] PDF
PD_EA_8904.pdf

Download (58kB)

Abstract

Force Measurements On Four Nose Configurations With Cylindrical After body Were Performed In 0.3m Wind Tunnel In The Mach Number Range Of 0.5 To 0.8 And Angle Of Incidence -4 To 14°.From Analysis Of Aerodynamic Data, It Was Observed That The Bulbous Nose Configuration Was The Optimum Configuration With Drag Penalty.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Nose configurations; After body; Mach number; Force - measurements.
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 90 not found.
Date Deposited: 27 Nov 2012 04:23
Last Modified: 27 Nov 2012 04:23
URI: http://nal-ir.nal.res.in/id/eprint/11342

Actions (login required)

View Item View Item