Balakrishna, S and Niranjana, T and Rajan, SR (1992) A rotary derivative rig for FMCD low speed tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (4Mb) |
Abstract
Rotary derivatives of a flight vehicle provide insight into13; its spin characteristics.The rotary derivative data can be13; generated for scaled aerodynamic models by coning motion at13; non-dimensional spin rates in the range of 0 to +/-0.313; at typical spin velocities. This document details the design of a rotary derivative rig for NAL FMCD's variable low speed (0-60 m/s) wind tunnel.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Rotary rig;Dynamic stability derivatives spin studies;Wind tunnel testing;Rotational aerodynamics |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 08 Aug 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1700 |
Actions (login required)
| View Item |
