Umakant, J and Krishnamurthy, M (1993) An Experimental Study On The Aerodynamic Effects Of Flare On An Axisymmetric Body. Technical Report. NAL, Bangalore.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
PD_EA__9302.pdf Download (64kB) |
Abstract
A Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, Typical Of Missile Configurations . Measurements Have Been Made Of The Longitudinal Aerodynamic Characteristics Of The Model For Angles Of Attack Upto 20 Deg . And Mach Numbers Ranging From 0.5 To 3.0. Flares Of Angles 5° , 10 ° , 15° And 20° At Three Axial Positions Have Been Considered In The Study. Test Results Have Been Presented In The Form Of Tables And Aerodynamic Characteristic Plots For Typical Subsonic, Transonic And Supersonic Mach Numbers Are Included .
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aerodynamic characteristics; flare; Axisymmetric body |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 08 Aug 2012 10:00 |
| Last Modified: | 08 Aug 2012 10:00 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10770 |
Actions (login required)
 |
View Item |
