1-2 of 2 Books
Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
By Richard M. Wood
Two experimental supercritical laminar-flow-control swept-wing airfoils
Two experimental supercritical laminar-flow-control swept-wing airfoils
By Dennis O. Allison