• 제목/요약/키워드: Composite numbers

검색결과 144건 처리시간 0.027초

연속섬유강화 플라스틱 복합재료의 반구형 압축성형성에 관한 연구 (A Study on the Hemisphere-Type Compression Molding for Continous Fiber-Reinforced Polymeric Composites)

  • 임용진;오영준;김이곤
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 1999년도 추계학술발표대회 논문집
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    • pp.149-153
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    • 1999
  • During a hemisphere-type compression molding, the wrinkles are caused by complex stress condition. It is very important to clarify the degree of wrinkles in order to have good products. In this paper, the effects of numbers of needling and initial area on the degree of wrinkles are studied. the degree of wrinkle is expressed as nonhomogeneity.

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Extended Central Composite Designs with the Axial Points Indicated by Two Numbers

  • Kim, Hyuk-Joo
    • Communications for Statistical Applications and Methods
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    • 제9권3호
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    • pp.595-605
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    • 2002
  • The central composite design is widely used for estimating second order response surfaces. This type of design is composed of $2^k$ factorial points, axial points and center points. In this paper, we suggest a version of central composite design where the positions of the axial points are indicated by two numbers, and study properties of this design. We obtain the variances and covariances of the estimators of the regression coefficients. Conditions are obtained for this design to be orthogonal and rotatable. This design is compared with other designs on the basis of efficiency.

복합재 원통쉘의 비틀림좌굴 거동 (Buckling Behavior of Composite Cylindrical Shells Under Torsion)

  • 강인식;이영신
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2000년도 추계학술발표대회 논문집
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    • pp.9-12
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    • 2000
  • This paper deals with the torsional buckling behavior of plain weave GFRP composite cylindrical shells having comparatively small length-to-diameter ratio. Boundary conditions corresponding to clamped ends and simply supported ends are considered. Torsional buckling loads and circumferential mode numbers according to the variation of shell length-to-radius ratio are conformed. To verify the availability of the theoretical results, comparison with the theoretical and experimental results are made.

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유효강우량 산정을 위한 곡선번호방법의 적용성 (Validity of Runoff Curve Number Method for Estimating of Effective Rainfall)

  • 윤태훈
    • 물과 미래
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    • 제24권2호
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    • pp.97-108
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    • 1991
  • 유역의 수문학적 토양피복형으로부터 유역 또는 합성곡선번호를, 강우-유출기록으로부터 관측곡선 번호를, 관측곡선번호의 중앙치로서 중위유선번호를 산정하였다. 유출기록을 기준으로 평가할 경우 AMC-II조건의 CN-II에 의하면 과소하게, AMC-III조건의 CN-III에 의하면 과대하게 유효강우량이 산정된다. 따라서 유효강우량산정의 개선방안으로 CN-II와 CN-III의 중간값인 조정곡선번호가 정의될 수 있다. 중위곡선번호에 의하여 산정된 유출이 관측치에 가장 근접하게 되는 점을 감안하면 계측유역의 대표곡선번호로서 중위곡선번호가 사용될 수 있다.

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THE SUM OF SOME STRING OF CONSECUTIVE WITH A DIFFERENCE OF 2k

  • LEE, SOUNGDOUK
    • Journal of applied mathematics & informatics
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    • 제37권3_4호
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    • pp.177-182
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    • 2019
  • This study is about the number expressed and the number not expressed in terms of the sum of consecutive natural numbers with a difference of 2k. Since it is difficult to generalize in cases of onsecutive positive integers with a difference of 2k, the table of cases of 4, 6, 8, 10, and 12 was examined to find the normality and to prove the hypothesis through the results. Generalized guesswork through tables was made to establish and prove the hypothesis of the number of possible and impossible numbers that are to all consecutive natural numbers with a difference of 2k. Finally, it was possible to verify the possibility and impossibility of the sum of consecutive cases of 124 and 2010. It is expected to be investigated the sum of consecutive natural numbers with a difference of 2k + 1, as a future research task.

Vibration of angle-ply laminated composite circular and annular plates

  • Mercan, Kadir;Ebrahimi, Farzad;Civalek, Omer
    • Steel and Composite Structures
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    • 제34권1호
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    • pp.141-154
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    • 2020
  • In the present paper, free vibration analysis of angle-ply laminated composite annular and circular plates is performed by numerical methods. First-order shear deformation plate theory is used for kinematic relations. The related governing equations of motion are discretized via differential quadrature and discrete singular convolution methods. Frequency values are obtained for different lamina scheme, thickness-to-radius ratio, and mode numbers. The advantages and accuracy of these two methods are also tested in detail.

FACTORIZATION IN THE RING h(ℤ, ℚ) OF COMPOSITE HURWITZ POLYNOMIALS

  • Oh, Dong Yeol;Oh, Ill Mok
    • Korean Journal of Mathematics
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    • 제30권3호
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    • pp.425-431
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    • 2022
  • Let ℤ and ℚ be the ring of integers and the field of rational numbers, respectively. Let h(ℤ, ℚ) be the ring of composite Hurwitz polynomials. In this paper, we study the factorization of composite Hurwitz polynomials in h(ℤ, ℚ). We show that every nonzero nonunit element of h(ℤ, ℚ) is a finite *-product of quasi-primary elements and irreducible elements of h(ℤ, ℚ). By using a relation between usual polynomials in ℚ[x] and composite Hurwitz polynomials in h(ℤ, ℚ), we also give a necessary and sufficient condition for composite Hurwitz polynomials of degree ≤ 3 in h(ℤ, ℚ) to be irreducible.

On buckling analysis of laminated composite plates using a nonlocal refined four-variable model

  • Shahsavari, Davood;Karami, Behrouz;Janghorban, Maziar
    • Steel and Composite Structures
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    • 제32권2호
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    • pp.173-187
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    • 2019
  • This study is concerned with the stability of laminated composite plates modelled using Eringen's nonlocal differential model (ENDM) and a novel refined-hyperbolic-shear-deformable plate theory. The plate is assumed to be lying on the Pasternak elastic foundation and is under the influence of an in-plane magnetic field. The governing equations and boundary conditions are obtained through Hamilton's principle. An analytical approach considering Navier series is used to fine the critical bucking load. After verifying with existing results for the reduced cases, the present model is then used to study buckling of the laminated composite plate. Numerical results demonstrate clearly for the first time the roles of size effects, magnetic field, foundation parameters, moduli ratio, geometry, lay-up numbers and sequences, fiber orientations, and boundary conditions. These results could be useful for designing better composites and can further serve as benchmarks for future studies on the laminated composite plates.

항공기 구조물에서 FRP를 이용한 보강부재의 피로수명에 대한 연구 (A study on fatigue life of aluminum plate reinforced with FRP in aircraft structure)

  • 박원조;허정원;이광영
    • 한국해양공학회지
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    • 제11권3호
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    • pp.69-75
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    • 1997
  • A A12024-T3 plate has been reinforced with AFRP to be a Hybrid-Composite, APAL. The fatigue life of the APAL has been investigated. The effects of bonding surface, numbers of AFRP bonded and AFRP orientation on fatigue life have been compared with A12024-T3 plate. Fatigue life of APAL has been remarkedly increased compared with that of A12024-T3 plate. The fatigue life has depended on bonding surface and AFRP orientation, but no relationship could be found with numbers of AFRP laminates.

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적층 복합재료를 사용한 곡면형 작동기의 성능 예측을 위한 대규모 수치해석 연구 (Large Scale Numerical Analysis for the Performance Prediction of Multilayered Composite Curved Actuator)

  • 정순완;황인성;김승조
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2003년도 추계학술발표대회 논문집
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    • pp.167-170
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    • 2003
  • In this paper, the electromechanical displacements of curved actuators using laminated composites are calculated by finite element method to design the optimal configuration of curved actuators. To predict the pre-stress in the device due to the mismatch in coefficients of thermal expansion, the carbon-epoxy and glass- epoxy as well as PZT ceramic is also numerically modeled by using hexahedral solid elements. Because the modeling of these thin layers causes the numbers of degree of freedom to increase, large-scale structural analyses are performed in a cluster system in this study. The curved shape and pre-stress in the actuator are obtained by the cured curvature analysis. The displacement under the piezoelectric force by an applied voltage is also calculated to compare the performance of curved actuator. The thickness of composite is chosen as design factor.

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