On the use of small scale aircraft models for dynamic wind tunnel investigation of stability and control-Reference-Cited by-同舟云学术

On the use of small scale aircraft models for dynamic wind tunnel investigation of stability and control

Published:1987-10 Issue:4 Volume:9 Page:190-197
ISSN:0142-3312
Container-title:Transactions of the Institute of Measurement and Control
language:en
Short-container-title:Transactions of the Institute of Measurement and Control

Author:

Cook M.V.¹

Affiliation:

1. College of Aeronautics, Cranfield Institute of Technology, Cranfield, Beds. England, MK43 OAL

Abstract

An experimental facility for the dynamic investigation of the stability and control characteristics of small scale model aircraft in a wind tunnel is described. Some typical results for a conventional and unconventional aircraft configuration are presented.

Publisher

SAGE Publications

Subject

Instrumentation

Link

http://journals.sagepub.com/doi/pdf/10.1177/014233128700900405

Reference4 articles.

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