Body and canard effects on an attached-flow maneuver wing at Mach 1.62 / James L. Pittman and David S. Miller, William H. Mason.Jimmy L. Pittman1984EN
Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / A. Warner Robins, Milton Lamb, and David S. Miller, Langley Research Center.A. Warner. Robins1979EN
The Canary Islands, Their History, Natural History and Scenery, an Account of an Ornithologist's Camping Trips in the Archipelage, by David A. Bannerman...David Armitage Bannerman1922EN