Characteristics of trim, drag, pitch damping, and longitudinal stability are presented; theoretical comparisons of lift and longitudinal stability and experimental results from similar configuration are included.
Aerodynamic characteristics over mach number range of 1.40 to 2.78 of rocket propelled airplane configuration having low 52.5° delta wing and unswept horizontal tail
NASA -- Tech Note
1961
26 pages
Article (Journal)
English
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