Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Model Having a 60 Degree Delta Wing and Low Swept Horizontal Tail (1955)
NASA Technical Reports Server (NTRS) · leaf 33
MCA RM L55F27 32 … Figure 15-- Comparison between stability characteristics of present test model and high-tail model of reference 1 at M 555 0.9.
NASA Technical Reports Server (NTRS)
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