Peck, Robert F. Results of rocket model test of an airplane configuration having an arrow wing and slender flat-sided fuselage: lift, drag, longitudinal stability, lateral force, and jet effects at Mach numbers between 1.0 and 2.3, report, February 21, 1956; (https://digital.library.unt.edu/ark:/67531/metadc62413/m1/1/: accessed July 19, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; .