Author:
QIU Jiahui,YANG Chen,ZHANG Wenqiang,ZHANG Min,DU Juan
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Reference36 articles.
1. SAE International. A current assessment of the inlet/engine temperature distortion problem. Warrendale: SAE International; 1991. Report No.: ARD50015.
2. Hot gas environment around STOVL aircraft in ground proximity. II - Numerical study;Tafti;J Aircr,1992
3. Childs J H, Kochendorfer F D, Lubick R J, et al. Stall and flame-out resulting from firing of armament. Washington, D.C.: NACA; 1955. Report No.: NACA RM E55E25.
4. Lucy B, Reed J. A survey of turbine engine temperature distortion generator requirements and concept trade study. Reston: AIAA; 2011. Report No.: AIAA-2011-5969.
5. A numerical simulation capability for analysis of aircraft inlet-engine compatibility;Hale;J Eng Gas Turbines Power,2006