The invention relates to a ground test method and
system for a
convective heat transfer coefficient of an aircraft outer
skin, belongs to the technical field of aircraft heat dissipation, and aims to solve the problem that the
convective heat transfer coefficient of the aircraft outer
skin is difficult to test. The test method comprises the following steps: building a test
system according to a test principle; determining a measuring point and calibrating a
thermocouple; according to the estimated heat exchange capacity of the
skin test piece, the power of a heating piece is set; the wind tunnel performs blowing test at the maximum
wind speed to monitor whether the test
system operates normally; setting an
attack angle and a sideslip angle of the
skin test piece, and feeding the five-axis
servo control system to a specified position; setting a wind tunnel operation mach number and wind tunnel operation; a power supply and a PLC temperature controller in the
test platform are started, and the test system operates; judging whether the test system is in a balanced state or not according to the temperature data displayed by the temperature
data collector, and calculating a
convective heat transfer coefficient; and adjusting the Mach number of the wind tunnel and the
attack angle and sideslip angle of the
skin test piece to enter the next test working condition, and repeating the steps S5-S8.