航空学报2025，Vol.46Issue(8)：162-176,15.DOI:10.7527/S1000-6893.2024.31233
考虑巡航攻角的三维内转进气道设计
Design of 3D inward-turning inlet considering cruising angle of attack
摘要
Abstract
Air-breathing hypersonic vehicles with the head intake system typically cruise at a specific angle of attack for higher lift-to-drag characteristics.However,this can cause the 3D inward-turning inlet,designed without consider-ing the angle of attack,to operate at off-design conditions for extended periods,which results in a noticeable decline in inlet performance.To solve this problem,the Local-Turning Osculating Cones(LTOCs)method is extended from ex-ternal flow to internal flow,and a 3D inward-turning inlet design method considering the cruising angle of attack is then proposed.In this method,the inward-turning inlet is divided into the shock-based and pressure-based segments,de-rived by specifying the incident 3D shock wave and the streamwise wall pressure distributions in each stream surface respectively.Numerical results demonstrate that the proposed method can accurately reproduce the preassigned shock waves and internal flowfield at Mach number 6,27 km altitude,and 4° angle of attack,resulting in full mass flow capture.Compared with the inlet design without considering the angle of attack,the design considering the cruising angle of attack can improve the inviscid mass-flow-capture coefficient and the inviscid total pressure recovery coeffi-cient at the throat section by 1.94%and by 6.56%,respectively,when the compression performances of two inlets are essentially identical.Under the viscous conditions,the mass-flow-capture coefficient is augmented by 1.90%,the total pressure recovery coefficient at the throat section is enhanced by 6.69%,and the total pressure recovery coeffi-cient at the isolator's exit section is elevated by 7.13%.关键词
高超声速/内转进气道/巡航攻角/流量捕获/总压恢复Key words
hypersonic/inward-turning inlet/cruising angle of attack/mass-flow-capture/total pressure recovery分类
航空航天引用本文复制引用
郑晓刚,胡占仓,蔡泽君,施崇广,朱呈祥,尤延铖..考虑巡航攻角的三维内转进气道设计[J].航空学报,2025,46(8):162-176,15.基金项目
国家自然科学基金(U21B6003,12202372) （U21B6003,12202372）
中国博士后科学基金(2022M712653) （2022M712653）
