Blanchard, Willard S. Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model, report, January 1, 1953; (https://digital.library.unt.edu/ark:/67531/metadc65341/m1/1/: accessed October 21, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; .