Support system for supersonic speed inlet direct connection wind tunnel test and design method

The invention discloses a support system and a design method for a supersonic speed inlet direct connection wind tunnel test, and relates to the field of high-speed aerodynamic test equipment design, and the system comprises a support platform which is connected with a releasing mechanism frame of a wind tunnel; the model supporting device is arranged above the supporting platform and is close to the upstream side in the airflow direction; the engine pedestal is arranged above the supporting platform and is close to the downstream side in the airflow direction; the supporting platform is provided with a turning table used for meeting the throwing distance in the downstream direction along the airflow direction. According to the supporting system for the supersonic inlet direct connection wind tunnel test and the design method, the supporting system adopts a modular structure, a test system suitable for the supersonic inlet direct connection wind tunnel test and a leading air inlet duct test can be convenientl