• Title/Summary/Keyword: 지능 포탄

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Study of Estimation Model for Wartime Stockpile Requirement of Intelligent Ammunition against Enemy Armored Vehicles (장갑차량 공격용 지능형 포탄의 전시 소요량 산정 모형에 관한 연구)

  • Cho, Hong-Yong;Chung, Byeong-Hee
    • Journal of the military operations research society of Korea
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    • v.34 no.2
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    • pp.143-162
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    • 2008
  • This paper aims to formulate the method of estimating the wartime stockpile requirement of 155mm self-propelled artillery including intelligent ammunition for armored vehicles, currently being developed. The usual method of utilizing war-game simulation results in considerable margins in expected occupancy ratio between ground forces and air forces for each weapon system for armored vehicles. Also, the method tends to produce excessive output greater than the minimal stockpile requirements; therefore, the study aims to overcome limitations like these by the allocation method for each weapon system according to targets. This allocation method is better than war-game simulation method.

A study on establishing the aerodynamic database though the external flow method of a rotating vehicle (회전 운동하는 비행체의 외부 유동장 해석을 통한 공력데이터베이스 구축 연구)

  • Kang, Tae-Woo;Ahn, Jong-Moo;Lee, Hee-Rang;Choi, Jae-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.8
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    • pp.41-47
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    • 2017
  • With the introduction of new technologies, ground weapons have led to the development of artificial intelligence and the attention of major developed countries. In this study, CFD was performed through the BLU-103 model to obtain aerodynamic data for aircraft that are subjected to rotational motion. To simulate the steady-state of a rotating body, the body was fixed and the principle of rotating the body by rotating the surrounding air was used. In order to examine the aerodynamic feasibility of the rotating aircraft, the analysis was carried out at intervals of $30^{\circ}$ angle from $0^{\circ}$ to $90^{\circ}$ for the simple shape and the side slip angle. It was confirmed that the drag coefficient for the simple model satisfies the quantitative results of 1.0 ~ 1.2 through CD presented in "Drag Book". The aerodynamic data was constructed by applying the valid input verified through the simple type analysis conditions to the actual shape, and the tendency was analyzed. The analysis confirmed that CX, CZ and CY increase not only in the simple model but also in the rotation of the actual model. Especially, the influence of CZ was judged to have contributed to the flight.