Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel

Abstract

An aerodynamic force and moment measurement was conducted in JF12 long-test-duration detonation-driven shock tunnel of Institute of Mechanics, Chinese Academy of Sciences. The test duration of JF12 is 100–130ms. The nominal Mach number is 7.0 and the exit diameter of the contoured nozzle is 2.5m. The total enthalpy is 2.5MJ/kg which duplicates the hypersonic flight conditions of Mach number 7.0 at 35km altitude. The test model is the standard aerodynamic force model of 10° half-angle sharp cone. The length of the test model is 1500mm and the weight is 57kg. The aerodynamic forces were measured with a six-component strain balance. The angles of attack were set to be −5°, 0°, 5°, 10° and 14°, respectively. The experimental results show that in the 100–130ms test duration, the signals of strain balance have 3–4 complete vibration cycles. So, the aerodynamic forces and moments can be obtained directly by averaging the signals of balance without acceleration compensation. The force measurement error of repeatability of JF12 is less than 2%. The aerodynamic force coefficients of JF12 are in good agreement with those of conventional hypersonic wind tunnels. For this test model at Mach number 7.0 and total enthalpy of 2.5MJ/kg, the real-gas effects on aerodynamic force characteristics are not very evident.