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A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels

IR@NAL: CSIR-National Aerospace Laboratories, Bangalore

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Title A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels
 
Creator Sundaramurthy, H
Narayana, T
 
Subject Aerodynamics
 
Description A free-oscillation test rig has been developed for measuring pitch- or yaw-damping derivatives of sting-mounted models in a trisonic wind tunnel. The rig is limited in applicability to sting-mounted models with moderate fineness ratios and with fairly aft centers of rotation. Results of evaluation testing of the rig with a 25 deg cone model are in good agreement with published data.
 
Publisher Aeronautical Society of India
 
Date 1976-05
 
Type Journal Article
PeerReviewed
 
Identifier Sundaramurthy, H and Narayana, T (1976) A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels. Journal of Aeronautical Society of India, 28 . pp. 227-230.
 
Relation http://nal-ir.nal.res.in/3847/