Raymond C Savin

Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28

Thomas J Wong, Raymond C Savin, 1956 .

Approximate methods for calculating the flow about nonlifting bodies of revolution at high supersonic airspeeds

Raymond C Savin, A J Eggers, 1951 .