التفاصيل البيبلوغرافية
العنوان:
Effect of Injection Mach Number on Penetration in a Supersonic Crossflow
المؤلفون:
Guang-xin Li , Mingbo Sun , Yuan Liu , Yu-Hui Huang , Jiangfei Yu , Guoyan Zhao , Chang-hai Liang
المصدر:
AIAA Journal . 58:1216-1226
بيانات النشر:
American Institute of Aeronautics and Astronautics (AIAA), 2020.
سنة النشر:
2020
مصطلحات موضوعية:
020301 aerospace & aeronautics , Materials science , Astrophysics::High Energy Astrophysical Phenomena , Aerospace Engineering , 02 engineering and technology , Penetration (firestop) , Mechanics , Boundary layer thickness , 01 natural sciences , Compressible flow , 010305 fluids & plasmas , Vortex , Physics::Fluid Dynamics , Transverse plane , symbols.namesake , 0203 mechanical engineering , Mach number , 0103 physical sciences , Empirical formula , symbols , High Energy Physics::Experiment , Supersonic speed , Astrophysics::Galaxy Astrophysics
الوصف:
For a transverse gaseous jet in supersonic crossflows, the empirical formula implies that the jet penetration height will monotonically increase with the injection Mach number under a certain cross...
تدمد:
1533-385X
URL الوصول:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5b3a58308bdd1fef370fecabdc21b3e https://doi.org/10.2514/1.j058580
رقم الأكسشن:
edsair.doi...........f5b3a58308bdd1fef370fecabdc21b3e
قاعدة البيانات:
OpenAIRE
