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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

The effect of altitude on cooling

Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines 1: capacity and economy

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


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