A rotary derivative rig for FMCD low speed tunnel

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: 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

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