• 대한수학회보
• /
• 제54권2호
• /
• pp.679-686
• /
• 2017

The present paper is devoted to self-adjoint cyclically compact operators on Hilbert-Kaplansky module over a ring of bounded measurable functions. The spectral theorem for such a class of operators is given. We use more simple and constructive method, which allowed to apply this result to compact operators relative to von Neumann algebras. Namely, a general form of compact operators relative to a type I von Neumann algebra is given.

• 대한수학회논문집
• /
• 제35권2호
• /
• pp.547-563
• /
• 2020

We define a left quotient as well as a right quotient of two bounded operators between Hilbert spaces, and we parametrize these two concepts using the Moore-Penrose inverse. In particular, we show that the adjoint of a left quotient is a right quotient and conversely. An explicit formulae for computing left (resp. right) quotient which correspond to adjoint, sum, and product of given left (resp. right) quotient of two bounded operators are also shown.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2003년도 The Fifth Asian Computational Fluid Dynamics Conference
• /
• pp.240-242
• /
• 2003

A method for performing two-dimensional lift-constraint drag minimization in inviscid compressible flows on unstructured meshes is developed. Sensitivities of objective function with respect to the design variables are efficiently obtained by using a continuous adjoint method. In addition, parallel algorithm is used in multi-point design optimization to enhance the computational efficiency. The characteristics of single-point and multi-point optimization are examined, and the comparison of these two method is presented.

• Journal of applied mathematics & informatics
• /
• 제5권3호
• /
• pp.669-690
• /
• 1998

In this paper we develop a new theory of adjoint and symmetric method in the class of general implicit one-step fixed-stepsize methods. These methods arise from simple and natral def-initions of the concepts of symmetry and adjointness that provide a fruitful basis for analysis. We prove a number of theorems for meth-ods having these properties and show in particular that only the symmetric methods possess a quadratic asymptotic expansion of the global error. In addition we give a very simple test to identify the symmetric methods in practice.

• 대한수학회보
• /
• 제60권4호
• /
• pp.1025-1034
• /
• 2023

Let U be the restricted quantized enveloping algebra Ũ_q(𝖘𝖑₂) over an algebraically closed field of characteristic zero, where q is a primitive 𝑙-th root of unity (with 𝑙 being odd and greater than 1). In this paper we show that any indecomposable submodule of U under the adjoint action is generated by finitely many special elements. Using this result we describe all ideals of U. Moreover, we classify annihilator ideals of simple modules of U by generators.

• Kyungpook Mathematical Journal
• /
• 제6권2호
• /
• pp.53-57
• /
• 1965

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2009년 춘계학술대회논문집
• /
• pp.57-65
• /
• 2009

An efficient and high-fidelity design approach for wing-body shape optimization is presented. Depending on the size of design space and the number of design of variable, aerodynamic shape optimization process is carried out via different optimization strategies at each design stage. In the first stage, global optimization techniques are applied to planform design with a few geometric design variables. In the second stage, local optimization techniques are used for wing surface design with a lot of design variables to maintain a sufficient design space with a high DOF (Degree of Freedom) geometric change. For global optimization, Kriging method in conjunction with Genetic Algorithm (GA) is used. Asearching algorithm of EI (Expected Improvement) points is introduced to enhance the quality of global optimization for the wing-planform design. For local optimization, a discrete adjoint method is adopted. By the successive combination of global and local optimization techniques, drag minimization is performed for a multi-body aircraft configuration while maintaining the baseline lift and the wing weight at the same time. Through the design process, performances of the test models are remarkably improved in comparison with the single stage design approach. The performance of the proposed design framework including wing planform design variables can be efficiently evaluated by the drag decomposition method, which can examine the improvement of various drag components, such as induced drag, wave drag, viscous drag and profile drag.

• 한국항공우주학회지
• /
• 제36권2호
• /
• pp.99-104
• /
• 2008

본 연구에서는 신경망에 기반한 불확실성 모델을 이용하여 전투기 날개 형상의 강건 최적 설계를 수행하였다. 불확실성 모델을 구축하기 위하여 공력성능과 이들의 민감도 정보를 중심합성법으로 선정된 실험점에서 구하였으며, 이 때 3차원 오일러 방정식과 adjoint변수방법이 사용되었다. 또한 비선형성 모사능력이 뛰어난 신경망모델을 이용함으로써 공력성능계수의 민감도 정보를 효율적이고 정확하게 예측하는 것이 가능하였다. 이와 같은 방법으로 구하여진 강건 최적 설계 결과로부터, 불확실성 모델의 변동과 신뢰도 수준의 변화가 증가할수록 목적함수 및 제약조건에 대한 강건성이 향상되는 것을 확인할 수 있었다.

• Smart Structures and Systems
• /
• 제21권4호
• /
• pp.449-467
• /
• 2018

In this paper, a theoretical and numerical study on bridge simultaneous damage detection procedure for identifying both the system parameters and input excitation mass, are presented. This method is called 'Adjoint Variable Method' which is an iterative gradient-based model updating method based on the dynamic response sensitivity. The main advantage of proposed method is inclusion of an analytical method to augment the accuracy and speed of the solution. Moving mass is a model which takes into account the inertia effects of the vehicle. This interaction model is a time varying system and proposed method is capable of detecting damage in this variable system. Robustness of proposed method is illustrated by correctly detection of the location and extension of predetermined single, multiple and random damages in all ranges of speed and mass ratio of moving vehicle. A comparison study of common sensitivity and proposed method confirms its efficiency and performance improvement in sensitivity-based damage detection methods. Various sources of errors including the effects of measurement noise and initial assumption error in stability of method are also discussed.

• 조명전기설비학회논문지
• /
• 제15권5호
• /
• pp.34-40
• /
• 2001

본 논문에서는 화력발전소 보일러 운전원 근무실 소음제어를 위하여 협대역 능동소음 제어시스템을 제안하였다. 제안된 시스템은 기준입력으로 구형파를 사용하여 기본파는 물론 고조파까지 한꺼번에 제어할 수 있게 하였으며, adjoint LMS 알고리즘을 사용하여 기존의 filtered-X LMS 알고리즘을 사용한 경우보다 계산량을 줄였다. 컴퓨터 시뮬레이션 결과, 기존의 광대역 능동소음 제어시스템에 비해 훨씬 작은 자수의 적응 필터를 사용하였으나, 더 우수한 특성을 보였다.