Comparative Flow Field Analysis of Boundary Layer Diverter Intake and Diverterless Supersonic Intake Configuration
فایل این مقاله در 7 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
تاریخ نمایه سازی: 18 دی 1400
چکیده مقاله:
کلیدواژه ها:
نویسندگان
Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology, H-۱۲, Islamabad, Pakistan
Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology, H-۱۲, Islamabad, Pakistan
Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology, H-۱۲, Islamabad, Pakistan
Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology, H-۱۲, Islamabad, Pakistan
Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology, H-۱۲, Islamabad, Pakistan