Aircraft ventilation force measurement wind tunnel test device and installation method and test method thereof

• Main Authors: SHAO SHUAI, ZHAO QING, NING RONGHUI, JIANG FUYUAN, WANG ZHIBIN, LI ZENGJUN, MENG YIFEI, CHANG LIXIA, HUANG YONG, ZHOU YOUTIAN
• Format: Patent
• Language: Chinese; English
• Published: 07.07.2023
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; MEASURING; PERFORMING OPERATIONS; PHYSICS; TESTING; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR; TRANSPORTING

The invention belongs to the technical field of aerodynamic wind tunnel tests, and discloses an aircraft ventilation force measurement wind tunnel test device and an installation method and a test method thereof. According to the aircraft ventilation force measurement wind tunnel test device and the...