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Effect of Variation of Conical Liner Apex Angle on Shaped Charge Performance

المصدر: المجلة الجامعة
الناشر: جامعة الزاوية - مركز البحوث والدراسات العليا
المؤلف الرئيسي: Ahmed, Khalifa Meftah (Author)
المجلد/العدد: مج22, ع2
محكمة: نعم
الدولة: ليبيا
التاريخ الميلادي: 2020
الشهر: يوينو
الصفحات: 1 - 12
رقم MD: 1263025
نوع المحتوى: بحوث ومقالات
اللغة: الإنجليزية
قواعد المعلومات: EduSearch, EcoLink, IslamicInfo, AraBase, HumanIndex
مواضيع:
كلمات المؤلف المفتاحية:
Shaped Charge | Standoff Distance | Jet Breakup | Penetration | Warhead Design
رابط المحتوى:
صورة الغلاف QR قانون
حفظ في:
LEADER 02434nam a22002657a 4500
001 2015631
041 |a eng 
044 |b ليبيا 
100 |9 672994  |a Ahmed, Khalifa Meftah  |e Author 
245 |a Effect of Variation of Conical Liner Apex Angle on Shaped Charge Performance 
260 |b جامعة الزاوية - مركز البحوث والدراسات العليا  |c 2020  |g يوينو 
300 |a 1 - 12 
336 |a بحوث ومقالات  |b Article 
520 |b The efficiency of conical linear shaped charge is estimated based on the penetration depth in a target material. Taking into consideration a significant number of parameters that affect the penetration depth, the optimization of the conical linear shaped charge parameters is a complex process.. In this study, the effect of varying conical liner apex angle is investigated using the SHARP code. A shaped charge with 29 mm charge caliber, conical liner base radius (cone base) is 28.3 mm and charge length is 72.5 mm. The study is carried out for cone apex angle 2α with values: 36°, 40°, 44°, 48°, 52°, 56°, 60° and 64°. The density law is used for estimating the penetration value. It was found that, as long as cone apex angle is increased, the value of target penetration is increased as well. This because the jet length is increased which is really the main factor in density law approach. But the behavior of jet length and penetration value is changing beyond the cone apex angle having the value of 53°, they start decreasing as cone apex angle is increased. This is because the distance travelled by the collapse liner element is increased so the jet velocity and its length are decreased and also because the decrease in the overall liner mass starts influence the jet formation in such a way that the jet mass decreases. 
653 |a هندسة الطيران  |a قانون الكثافة  |a المعلومات الجوية  |a البطانة المخروطية 
692 |b Shaped Charge  |b Standoff Distance  |b Jet Breakup  |b Penetration  |b Warhead Design 
773 |4 العلوم الإنسانية ، متعددة التخصصات  |6 Humanities, Multidisciplinary  |c 005  |e University Bulletin  |l 002  |m مج22, ع2  |o 0928  |s المجلة الجامعة  |v 022 
856 |u 0928-022-002-005.pdf 
930 |d n  |p y  |q n 
995 |a EduSearch 
995 |a EcoLink 
995 |a IslamicInfo 
995 |a AraBase 
995 |a HumanIndex 
999 |c 1263025  |d 1263025 

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