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absolute temperature ADVANCE RESTRICTED REPORT air shroud Aircraft Heaters Airesearch airplane speed altitude approximately arithmetic average Btu/hr ft2 cabin wall calculated calibration clothing correction cross-sectional area curve emissivity enthalpy entrance equation evaluated exhaust gas side fins ft/sec ft2 F gas and air gases heat exchanger heat flow heat loss heat meter heat transfer heat-meter heater shell hydraulic diameter inches inlet and outlet Investigation of Aircraft isothermal pressure drop lb/hr length magnitude Measured and Predicted Morrin NACA non-isothermal pressure drop obtained outlet ducts over-all thermal conductance percent pounds per hour Predicted Performance radiation rate of heat reference shown in figure STANFORD UNIVERSITY static pressure drop steel heater temperature of fluid thermal output thermal resistance thermocouples thermopile tion tube type heater unit thermal conductance ventilating air rate ventilating air side ventilating-air Viscosity weight rate