Method, device and equipment for reducing heat and drag of hypersonic aircraft and storage medium

• Main Authors: ZHU HONGWEI, LI BING, CHANG YAN, ZHANG DAQIAO, LI XUERUI, YANG XIAOYUN, WANG SHUNHONG, PAN LEFEI
• Format: Patent
• Language: Chinese; English
• Published: 19.01.2024
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; COSMONAUTICS; HELICOPTERS; PERFORMING OPERATIONS; TRANSPORTING

The embodiment of the invention provides a hypersonic aircraft heat and resistance reduction method, device and equipment and a storage medium, and the method comprises the steps: collecting target flight state data of an aircraft, the target flight state data comprising a flight Mach number and an attack angle number; target setting parameters corresponding to the target flight state data of the aircraft are obtained, and the target setting parameters comprise a shock wave rod size parameter, a reverse jet flow pressure ratio, a lateral jet flow pressure ratio and a lateral jet flow direction number; the target setting parameters of the aircraft are adjusted based on the target flight state data, the aerodynamic heat and resistance of the aircraft under the non-zero attack angle can be effectively reduced, the aerodynamic performance of the aircraft is improved, and the maneuverability is greatly improved. 本公开的实施例提供了一种高超声速飞行器降热减阻方法、装置、设备和存储介质，包括：采集飞行器的目标飞行状态数据，其中，目标飞行状态数据包括飞行马赫数和攻角数；获取与飞行器的目标飞行状态数据对应的目标设置参数，