NACA research memorandum RM (series). L57E14a. Aerodynamic heating and boundary-layer transition on 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 × 10° [with list of references]; by Benjamlne J. Garland, Andrew G. Swanson, and Katherine C. Speegle.