B. B. Estabrooks

Transonic-wing investigation in the Langley 8-foot high-speed tunnel at high subsonic Mach numbers and at a Mach number of 1.2: analysis of pressure distribution of wing-fuselage configuration having a wing of 45 degrees sweptback, aspect ratio 4, t

Donald L. Loving, Bruce B. Estabrooks, D. L. Loving, 1951 .