摘要
A typical blunt body such as Tianwen-1 Mars entry capsule suffers dynamic instability in supersonic regime.To investigate the unstable Mach range of flight and to confirm the design of aerodynamic shape and mass properties,a ballistic range test was carried out aiming at capturing supersonic dynamic characteristics of Tianwen-1.Aerodynamic coefficients of free-flight scaled models were derived by modified linear regression method based on position and attitude data,while the dynamic coefficients were established under the assumption of small angle linearization.The static moment coefficients and dynamic derivatives were identified thereafter.Results show that models in untrimmed configuration are dynamically unstable at certain Mach numbers,whereas models in trimmed configuration are dynamically stable at other Mach numbers tested.Both trimmed and untrimmed configurations are statically stable in all testing cases.
