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 25
24 NACA m L55F27 … P'igure 6.- Variation of trim characteristics with Mach number
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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