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302. NACA research memorandum RM (series). L57L02. Aerodynamic load distribution on 45° sweptback wing with leadingedge chord-extensions at transonic speeds. Including effects of spoiler-slot-deflector aileron [with list of references]; by James W. Schmeer, Charles F. Whitcomb, and F. E. West, jr.

303. NACA research memorandum RM (series). L57L04. Free-flight investigation at Mach numbers from 0.8 to 1.5 of effect of fuselage indentation on zero lift drag of 52.5° sweptback-wing-body configuration with symmetrically mounted stores on fuselage [with list of references]: by Sherwood Hoffman.