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202. NACA research memorandum RM (series). A58E21n. Forces and pitching moments on aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of effect of single-element roughness on boundary-layer flow [with list of references]; by Edward J. Hopkins, Stephen J. Keating, jr., and Richard R. Muhl.

205. NACA research memorandum RM (series). L58E26. Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of generalized missile model having rectangular wing at Mach number of 4.08 [with list of references]; by Fred M. Smith, Edward F. Ulmann, and Robert W. Dunning.