• Title/Summary/Keyword: 가변스팬

Search Result 6, Processing Time 0.019 seconds

Aerodynamic Characteristics of a Variable Span Wing Flying Inside a Channel I (Effects of Wing Aspect Ratio and Guideway) (채널 내를 비행하는 가변스팬 날개 공력특성 I (가로세로비 및 안내로 영향))

  • Han, Cheolheui
    • Journal of Aerospace System Engineering
    • /
    • v.10 no.4
    • /
    • pp.11-16
    • /
    • 2016
  • In this paper, an experimental study on the aerodynamic characteristics of a variable span wing flying inside a channel guideway is accomplished using wind tunnel testing. A variable span wing with a NACA 0012 airfoil section was fabricated and actuated using a linear servo motor. The aerodynamic effects of 1) wing aspect ratio, 2) ground effect, and 3) the gap between the wingtip and the wing fence were investigated. It was found that both ground effect and wing fence gap increased lift. Also, the wing fence gap does not significantly affect drag. Therefore, it was found that a variable span mechanism can be used as an effective high lift device when flap use is limited.

Aerodynamics and Flight Control of Air Vehicle with Variable Span Morphing Wing (가변스팬 모핑날개를 가진 비행체의 공력특성 및 비행 제어)

  • Bae, Jae-Sung;Hwang, Jai-Hyuk;Park, Sang-Hyuk;Kim, Jong-Hyuk
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.18 no.4
    • /
    • pp.1-8
    • /
    • 2010
  • In the aerospace field, the study on a morphing-wing is in progress to improve flight performance and perform multi flight mission. There are many concepts of morphing-wing such as camber-change, wing-twist, variable-span, and so on. In this study, the aerodynamic characteristics and flight control of an air vehicle with a variable-span morphing wing (VSMW) have been investigated. VSMW with symmetric span control(SSC) can increase cruising range of aircraft by reducing drag in various flight condition. VSMW with anti-symmetric span control(ASSC) can be used in the roll control of an aircraft. The flight control about pure rolling dynamic system and full dynamic system have been performed about the cruise missile.

Development and Flight Test of Variable-Camber and Variable-Chord Morphing Flap (가변캠버 가변시위 모핑 플랩의 개발 및 비행실험)

  • Jihyun Oh;Jae-Sung Bae;Hyun Chul Lee
    • Journal of Aerospace System Engineering
    • /
    • v.18 no.4
    • /
    • pp.34-42
    • /
    • 2024
  • This study developed a morphing technology applicable to unmanned aerial vehicles (UAVs) with diverse flight characteristics. Existing morphing technologies require additional mechanisms and driving devices, posing challenges in constructing features such as ribs and spars within the wing structure, leading to structural instability. To address this, we developed a Variable-Camber and Variable-Chord (VCC) morphing flap that could maintains a continuously transforming surface during deformation, altering both camber shape and chord length simultaneously. Furthermore, we conducted design and fabrication of UAV wings incorporating these morphing flaps, ensuring structural stability by developing specialized shapes. Furthermore, structural experiments were conducted to simulate flight loads, followed by actual flight tests to validate performances of both morphing mechanism and wings. Finally, wind tunnel tests were conducted to compare results with aerodynamic analysis, confirming the effective applicability of this morphing technology.

Aerodynamic Characteristics of a Variable-Span Wing Flying Inside a Channel II (Effect of Asymmetric Wing Extensions) (채널 내를 비행하는 가변스팬 날개 공력특성 II (비대칭 날개 펼침))

  • Han, Cheolheui
    • Journal of Aerospace System Engineering
    • /
    • v.10 no.3
    • /
    • pp.39-43
    • /
    • 2016
  • In this paper, a wind-tunnel test is accomplished to investigate the roll characteristics of a variable-span wing flying inside a channel. The factors that affect the roll characteristics of the wing were identified by analyzing the measured data; accordingly, when the wing is flying without both the ground and sidewall effects, the asymmetric wing extension causes the roll moment. Both the ground and the sidewall can increase the roll moment, but when the wing is affected by both the ground and the sidewall, the roll moment does not increase as much as the case where the wing is only affected by the ground. Also, the aerodynamic characteristics of the flying wing inside a channel are the nonlinear function of the wing height and the gap between the wingtip and the sidewall, both of which should be considered in a study of the stability and the flight control of the wing-in-ground effect of the vehicle flying inside a channel.

Flexible Unit Floor Plan of Off-Site Construction Housing Considering Long-Lasting Housing Certification System (장수명주택 인증을 고려한 OSC공법 주택의 가변형 평면계획 연구)

  • Lee, Ji-Eun;Roh, Jeong-Yeol;Kwon, Soo-Hye;Kim, Seung-Mo
    • Land and Housing Review
    • /
    • v.12 no.4
    • /
    • pp.103-117
    • /
    • 2021
  • With the current rapid changes in population and technology, the long-lastig housing certification system is a means of prolonging the physical and functional lifespan of a building. The certification requires differentiation between the structure and infill elements to allow for variability and ease of repairs. This works well with prefabricated houses so this study investigated the possibility of applying the long-lastig housing certification requirements to apartment construction using off-site construction (OSC) methods focused on the installation of bathrooms (plumbing and toilet) that differ from the traditional wet method. This study examined three different sized floor plans at 22 m2, 46 m2, and a combined one resulting in 69 m2. The larger 69 m2 plan utilized a removeable non-load bearing wall to increase flexibility in the layout of the floorplan. The apartments are constructed of steel reinforced concrete composite columns on a 9 m × 10.5 m grid with integrated slabs. The exterior and interior infill walls are all non-load bearing with some containing plumbing. This separation of the structure and infill walls can help meet some of the criteria in the long-lastig housing certification, particularly with the ease of repairs. Technologies that facilitate the replacement of infill elements that contain plumbing and other building services can benefit the nation by reducing carbon emissions and therefore tax incentives should be introduced to increase the adoption of the proposed construction methods.

A Numerical Study on the Apartment Structure Using Crossed Wide Girder (교차형 와이드 거더를 이용한 아파트구조의 수치해석적 연구)

  • Park, Jung-Hyun
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.8 no.5
    • /
    • pp.1186-1191
    • /
    • 2007
  • The study uses the crossed wide girder(waffle slab type) in apartment structural system comparing with existing shear wall system. The crossed wide girder will be able to secure the span of the longest which is possible with minimum slab thickness by not increasing the height. The research sees continuity arranges the crossed wide girder in schedule interval following the stress distribution. Namely, it is to make the interior space with the space without column and wall in the minimum height. In order to check the numerical value of this study which it interpreted the ductile frame system due to the crossed wide girder and existing shear wall system used the Midas Gen is a program which 3-dimension laterial force designs are possible. Analysis results, the crossed wide girder system is not disadvantageously laterial drift, drift ratio and deflection of slab compares with existing shear wall system. Also the whole concrete amount is similar existing shear wall system. The crossed wide girder is advantage which secure a architectal variability.

  • PDF