Large lift-to-drag ratio, high maneuverability, and good controllability are the basic performance for flight vehicles. Studying the rolling stability problems of a high lift-to-drag ratio aircraft is of great significance to the safety and control in maneuvering flight. The research on the static stability in the rolling direction of a HTV-2 like shape under a typical Mach number and attack angle was carried out. Similarly, by using Euler, laminar, turbulence and transition models, investigatio... 

【文章來源】：Aerospace China. 2020,21(03)

【文章頁數(shù)】：7 頁

【文章目錄】：
1 INTRODUCTION
2 NUMERICAL METHODS
    2.1 N-S Equations
    2.2 Dynamic Derivatives Identification Methods
3 NUMERICAL SIMULATION RESULTS OF FINNER
4 HTV-2 LIKE SHAPE AND GRID
5 NUMERICAL SIMULATION RESULTS AND ANALYSIS
    5.1 Steady Simulation
    5.2 Unsteady Simulation
6 CONCLUSIONS


【參考文獻(xiàn)】：
期刊論文
[1]Numerical Simulation of Unsteady Flow of Reentry Capsule[J]. MA Yuanhong,SHI Xiaotian,LV Meng,SHEN Qing.  Aerospace China. 2019(01)
[2]一種近空間高超聲速飛行器滾轉(zhuǎn)穩(wěn)定性研究[J]. 李乾,趙忠良,王曉冰,李玉平,馬上.  航空學(xué)報. 2018(03)
[3]類HTV-2橫側(cè)向穩(wěn)定性研究[J]. 高清,趙俊波,李潛.  宇航學(xué)報. 2014(06)



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