• 제목/요약/키워드: air force

검색결과 1,930건 처리시간 0.033초

수치해석을 이용한 부양실 설계변수에 관한 연구 (A Parametric Study on Design Variables of Lifting Chamber Using Numerical Simulation)

  • 전창수
    • 한국전산유체공학회지
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    • 제3권2호
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    • pp.52-64
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    • 1998
  • Numerical simulations on the flowfield of lifting chamber for Wing-In-Ground vehicle were performed using Fluent/UNS 4.2 software. The trend of lifting force in lifting chamber and parametric study of geometric and fluid variables were primarily investigated. Selected parameters for investigation are inlet velocity, height between chamber and water level, depth of the skirt, location of inlet, variaton of height at bow and stern. Also, air capturing capabilities from downstream of the propeller were evaluated at the air inlet. The lifting force was increased linearly with the increased of inlet velocity and nonlinearly with the decrease of height force was increased with increased depth. It turned out to have very minor effect on lifting force to change the location of air inlet for lifting chamber, installed on top surface. Tilting the vehicle when it was lifted, the lifting forces, generated in each case, showed no appreciable changes.

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유무인 협업을 활용한 고가치 공중 자산의 호위 전술 개발과 M&S를 활용한 효과적인 전력배치 방안 연구 (The Development of Air Escort Tactics for High-Value Airborne Assets Using Manned-Unmanned Teaming and the Study on Effective Force Disposition Using M&S)

  • 박명환;유승훈;오지현;설현주
    • 한국군사과학기술학회지
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    • 제25권4호
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    • pp.401-411
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    • 2022
  • As the role of high-value air assets(e.g., AWACS, JSTARS, Rivet Joint, E-2) becomes more critical in modern warfare, the air escort for these assets blocking attacks from any potential enemy fighter also becomes vital. Without the escort, the operations of the assets become restricted. However, such an escort is not always possible due to the limited flight time of the escort fighters. In this paper, we introduce an escort tactics for high-value air assets performed by the manned-unmanned teaming composed of a transport aircraft and UAVs(unmanned aerial vehicles). In this tactics, the transport aircraft plays the role of an aircraft carrier, which carries, launches, and retrieves the UAVs. The missions of UAVs in this tactics are to detect and engage enemy fighters. We also introduce the simulation result of this tactics to identify the UAVs' required capabilities and optimal maneuvering.

롱샷 무인기를 활용한 유무인 협업 공대공 전술 개발 (Manned-Unmanned Teaming Air-to-Air Combat Tactic Development Using Longshot Unmanned Aerial Vehicle)

  • 유승훈;박명환;황성인;설현주
    • 산업경영시스템학회지
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    • 제44권3호
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    • pp.64-72
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    • 2021
  • Manned-unmanned teaming can be a very promising air-to-air combat tactic since it can maximize the advantage of combining human insight with the robustness of the machine. The rapid advances in artificial intelligence and autonomous control technology will speed up the development of manned-unmanned teaming air-to-air combat system. In this paper, we introduce a manned-unmanned teaming air-to-air combat tactic which is composed of a manned aircraft and an UAV. In this tactic, a manned aircraft equipped with radar is functioning both as a sensor to detect the hostile aircraft and as a controller to direct the UAV to engage the hostile aircraft. The UAV equipped with missiles is functioning as an actor to engage the hostile aircraft. We also developed a combat scenario of executing this tactic where the manned-unmanned teaming is engaging a hostile aircraft. The hostile aircraft is equipped with both missiles and radar. To demonstrate the efficiency of the tactic, we run the simulation of the scenario of the tactic. Using the simulation, we found the optimal formation and maneuver for the manned-unmanned teaming where the manned-unmanned teaming can survive while the hostile aircraft is shot-downed. The result of this study can provide an insight to how manned aircraft can collaborate with UAV to carry out air-to-air combat missions.

BLDC 전동기의 동적 편심 및 전자기적 불평형력을 고려한 편심 회전자의 과도 동적 해석 (Transient Dynamic Analysis of a Dynamci Eccentric Rotor with Unbalanced Magnetic Forces in BLDC Motors)

  • 김태종;황상문;박노길
    • 소음진동
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    • 제10권3호
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    • pp.401-409
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    • 2000
  • Vibration of a BLDC motor is a coupled phenomenon between mechanical characteristics and magnetic origins through the motor air-gap. When a relative misalignment of rotor in the air-gap center exists on the assemblage it is considered to influence the motor system characteristics, depending on the degree of misalignment. The rotor-motor system used in a washing machine is modeled using FE-TM and a magnetic force of BLDC motor with radial rotor eccentricity is analyzed. And the transient whirl responses of a rotor system with relative misalignment in the motor air-gap are investigated considering mechanical origins and magnetic effects. Results show that rotor misalignment in the air-gap affect the vibration of the rotor-motor system.

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Optimal Placement of CRNs in Manned/Unmanned Aerial Vehicle Cooperative Engagement System

  • Zhong, Yun;Yao, Peiyang;Wan, Lujun;Xiong, Yeming
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제13권1호
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    • pp.52-68
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    • 2019
  • Aiming at the optimal placement of communication relay nodes (OPCRN) problem in manned/unmanned aerial vehicle cooperative engagement system, this paper designed a kind of fully connected broadband backbone communication topology. Firstly, problem description of OPCRN was given. Secondly, based on problem analysis, the element attributes and decision variables were defined, and a bi-level programming model including physical layer and logical layer was established. Thirdly, a hierarchical artificial bee colony (HABC) algorithm was adopted to solve the model. Finally, multiple sets of simulation experiments were carried out to prove the effectiveness and superiority of the algorithm.

반잠수압기형부방파제의 비선형파랑변형 및 동적거동에 관한 연구 (Nonlinear Wave Transformation and Dynamic Behaviors of Semi-Submerged Air-Chamber Floating Breakwater)

  • 김도삼
    • 한국항만학회지
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    • 제10권1호
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    • pp.25-36
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    • 1996
  • Generally, it is pointed out that a nonlinear analysis is needed to estimate accurately the water surface fluctuation and dynamic responses of a floating structure in case of large wave reflection. In this study, a frequency-domain method is applied and newly developed to analyze the nonlinear characteristics of the air-chamber floating breakwater. The air-chamber floating breakwater in this study can control well the wave transformation, motions of the structure and its natural frequency by adjusting the air depth in the chamber. Experiments are carried out to verify the numerical results. It is appeared that the mean water level is setup in the anti-node and setdown in the node, while the nonlinearity in wave profile is larger in the node than in the anti-node. Because of vertical mooring system, the sway, especially the time-independent nonlinear component, plays predominant role in the motion. On the other hand, the time-dependent component, as well as the time-independent one to the tensile force of mooring line contributes greatly, and the time averaged value presents tensional force oriented to the onshore side due drift force.

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도심항공모빌리티(UAM)의 군사적 운용방안에 관한연구 (A Study on the Military Operation of Urban Air Mobility (UAM))

  • 서강일;박상혁
    • 문화기술의 융합
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    • 제9권3호
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    • pp.287-292
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    • 2023
  • 미국 항공우주국(NASA)은 저고도의 공중을 새롭게 구축하고자 도시의 단거리 항공 운송 생태계를 새로운 개념의 도심항공모빌리티(Urban Air Mobility, UAM)을 제시하여 현재 UAM이라는 용어가 전 세계적으로 통용되고 있다. 이러한 패러다임은 우리나라 정부에서도 2025년까지 도심항공교통 서비스 상용화를 목표로 추진하고 있는 실정이며 더 나아가 급변하는 미래 작전환경 및 전장 공간의 확장으로 공중기동·수송능력 확보 필요성이 대두되고 있어 우리나라 군 조직에서도 필요성이 제기되는 부분이다. 즉, 본 연구는 미 공군의 'Agility Prime' 프로그램을 소개하여 군사적 필요성과 군사적 운용방안에 대해 제시하고자 출발한 연구이며 연구의 체계는 도심항공 모빌리티 배경 및 개념, 한국형 도심항공 모빌리티 발전 추세, 미 공군의 'Agility Prime' 프로그램 분석 순으로 구성하였으며 본 연구에 이어서 후속연구로 진행되길 기대한다.

A Computational Analysis of Air Entrainment with a Nip Roller

  • 이재용
    • 한국펄프종이공학회:학술대회논문집
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    • 한국펄프종이공학회 2002년도 추계학술발표논문집
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    • pp.81-90
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    • 2002
  • Air entrainment of a winding roll with a nip roller was studied numerically. The amount of air entrainment between two rotating rollers was obtained by solving lubrication equation, Reynolds equation, which neglect the existence of a web. However, the numerical model of this study included the web existence, therefore it considered the two lubricating air films between a winding roll and a web and also between a nip roller and the web. The pressure profiles and gap profiles of the two films were obtained by solving lubrication equation for the two air films and force balance equation of the web. Ballooning phenomenon was examined in terms of nip force, wrap angle, web stiffness, web speed, and web tension. This ballooning phenomenon caused by the back flow of the air film blocked by the nip roller. Air entrainment of the two numerical models was compared.

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A Study on the Functions of 𝜅𝜙-Bounded Variations

  • Sok, Young-U;Park, Jae-Keun
    • 충청수학회지
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    • 제2권1호
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    • pp.55-64
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    • 1989
  • In this paper, we study some properties of generalized function spaces of ${\kappa}$-, ${\phi}$-and ${\kappa}{\phi}$-bounded variations and general bounded variations.

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