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- The Use of Suction to Prevent Shock-Induced Separation in a Nozzle
- Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05
- Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form: Longitudinal and Lateral Control Characteristics
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04