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oaioai:nal-ir.nal.res.in:11390

Wind tunnel test studies on 1/7 scale NALLA-1 model

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Publication date
1 February 1992
Publisher
National Aerospace Laboratories

Abstract

Wind tunnel tests comprising of flow visualization and measurement of forces and moments have been carried out on a 1/7 scale model of the NAL Light Aircraft -(NALLA-1) and its variants in the open circuit wind tunnels at the Indian Institute of Science, Bangalore. Aerodynamic characteristics of the model derived from these tests are presented in this report

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Last time updated on 16/07/2013

This paper was published in National Aerospace Laboratories Institutional Repository.

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