Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections
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Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1957
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1956