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.
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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: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Rotary rig;Dynamic stability derivatives spin studies;Wind tunnel testing;Rotational aerodynamics |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 08 Aug 2006 |
| Last Modified: | 24 May 2010 04:13 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1700 |
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