Rajamurthy, MS and Rajan, SR and Basappa, - and Niranjana, T (1993) Estimation Of Longitudinal Moment Derivatives Of Missile Configuration Using Semi Free Flying Technique. Technical Report. NAL, Bangalore.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
PD_FC_9315.pdf Download (63kB) |
Abstract
A Semi-Free Dynamic Flying Test Technique Has Been Used To Estimate The Pitching Moment Derivatives Of A Missile Model. Wind Tunnel Tests Were Carried Out On A 1 :8 Scale Model Of PJ08 Missile Configuration. The Pitching Moment Derivatives Were Estimated From The Angular Motion Responses Of The Model To Doublet Input Using MLE Method. The Results Of Tests On Configuration 1 For Three CG Positions Are Detailed.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Semi-free Flying; Missile Configuration; Longitudinal Moment Derivatives |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 25 Sep 2012 04:59 |
| Last Modified: | 25 Sep 2012 04:59 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10983 |
Actions (login required)
 |
View Item |
