Milton Lamb

• A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70
• Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
• Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
• Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
• Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels
• Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
• Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86
• Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf