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- Combustion-engine temperatures by the sodium line-reversal method
- Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model
- Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model, Special Report
- The effect of air-passage length on the optimum fin spacing for maximum cooling
- Generalized selection charts for bombers powered by one, two, four, and six 3000-horsepower engines 1: capacity and economy
- Generalized selection charts for bombers with four 2000-horsepower engines
- Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines
- Effect of airplane design efficiency and engine economy on range
- Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines 1: capacity and economy
- The effect of altitude on cooling
- Turbulent-Heat-Transfer Measurements at a Mach Number of 3.03
- Turbulent-heat-transfer measurements at a Mach number of 1.62
- Turbulent-heat-transfer measurements at a Mach number of 2.06
- Turbulent-heat-transfer measurements at a Mach number of 0.87
- Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90
- Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05