Addendum to: Directional stability tests at M=1.57 on a 1/80 scale model of the Avro C-105 aircraft with certain modifications

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Addendum to: Directional stability tests at M=1.57 on a 1/80 scale model of the Avro C-105 aircraft with certain modifications

Entry/Object ID

3421

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Report - Technical

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Description

Factors affecting directional stability are reviewed in relation to the C-105 configuration. Flow visualization and force tests were carried out at M=1.57 on standard C-105 configuration and on 5 modifications involving ventral fins, wing fins, enlarged vertical tail and wing fences. The results of tests indicated in general favourable effects of four modifications on directional stability. Comparison with NACA data indicates satisfactory agreement.

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Date / Time Period: 6/28/57 Pages: 11 Author: J.A. Van Der Bliek Publisher: National Aeronautical Establishment Canada