Drag and Static Stability at Low Lift of Rocket-Powered Models of the Convair MX-1626 Airplane at Mach Numbers From 0.7 to 1.5
Description:
Report presenting flight testing on models of the proposed Consolidated Vultee Aircraft Corporation MX-1626 airplane with nacelles and without nacelles. Results regarding drag level, design modifications, dampening, trimming, and the use of ventral boosters are provided.
Date:
June 11, 1953
Creator:
Hall, James R. & Hopko, Russell N.
Item Type:
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Partner:
UNT Libraries Government Documents Department