Unsteady Two Dimensional Airloads Acting on Oscillating Thin Airfoils in Subsonic Ventilated Wind Tunnels / Joseph Fromme and Michael Golberg.Joseph. Fromme1978
Experimental aerodynamic characteristics for slender bodies with thin wings at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Michael H. Howell.Leland H. Jorgensen1976