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693. NACA research memorandum RM (series). E57F03. Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0 [with list of references]; by James F. Connors, J. Calvin Lovell, and George A. Wise.

699. NACA research memorandum RM (series). L57G30. Free-flight skin-temperature and surface-pressure measurements on highly polished nose having 100° total-angle cone and 10° hail-angle conical flare section up to Mach number of 4.08 [with list of references]; by Bernard Rushis and Aleck C. Bond.