Krishnamurthy, K (1989) Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel. Technical Report. NAL, Bangalore.
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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: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Nose configurations; After body; Mach number; Force - measurements. |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 27 Nov 2012 09:53 |
| Last Modified: | 27 Nov 2012 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11342 |
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