Dynamic longitudinal stability and control of tandem coupled bomber-fighter airplane models with rigid and pitch-free couplings
Description: Report presenting an investigation in the free-flight tunnel to determine the dynamic longitudinal stability and control characteristics of tandem-coupled bomber-fighter airplane models. Results regarding bomber alone tests, freely coupled combination, and rigidly coupled combination are provided.
Date: January 22, 1951
Creator: Granda, David C. & Hewes, Donald E.
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