Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 / Barrett L. Shrout, William A. Corlett, and Ida K. Collins.Barrett L. Shrout1979
1001 answers to your Florida garden questions Herbert S. Wolfe, John V. Watkins Thomas B. Mack, with drawings by Esther Coogle and Phil Calkins.Herbert S. Wolfe1962
Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 / Paige B. Burbank, Robert A. Newlander and Ida K. Collins.Paige B. Burbank1962