서지주요정보
풍동시험부의 벽면간섭 및 적응벽면 모형에 관한 수치적 연구 = Numerical study on wall interference and adaptive wall models for wind tunnel test section
서명 / 저자 풍동시험부의 벽면간섭 및 적응벽면 모형에 관한 수치적 연구 = Numerical study on wall interference and adaptive wall models for wind tunnel test section / 장병희.
발행사항 대전 : 한국과학기술원, 1996].
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소장정보

등록번호

8006212

소장위치/청구기호

학술문화관(문화관) 보존서고

DAE 96001

휴대폰 전송

도서상태

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반납예정일

리뷰정보

초록정보

Wall interference is one of the major obstacles to increase the model size and data accuracy. There have been many treatments for wall interference including interference correction and adaptive wall test section. The adaptive wall concept is an active means to remove wall interference and has been realized in two-dimensional steady flow testing. In order to be practiced in three-dimensional or unsteady testing, further research and development are required. The objective of this study is to suggest and verify a new adaptive wall model for unsteady two-dimensional test and steady three-dimension test. In this study, wind tunnel and free air tests are simulated by the numerical computation of Euler equations. In order to compare the ability of reducing wall interference, two classical correction methods and one measured-boundary-condition method are applied to test section result. By those correction methods, wall interference are reduced significantly, but less effective than those by adaptive wall. For the two-dimensional steady flow, The adaptive wall's ability of eliminating wall interference are evaluated from the point of view of flow speed, also. For two-dimensional unsteady flow, unsteady adaptation has never been realized until now. In the present study, practicable models are suggested and numerically verified to be effective in reducing unsteady wall interference. The necessary facts for their real application are discussed. Recently, two-flexible-walled adaptive wall test section is concluded adequate for three-dimensional test. But proper location of target line and pressure holes are critical to its success. In this study, a new adaptive algorithm which dispenses target line and dependency of pressure hole distribution is suggested. The optimum wall shape is achieved by two variable optimization which is composed of two base streamlines. The wall interference is reduced well in the optimized result which is not sensitive to the base streamlines. So, base streamlines can be obtained from numerical computation in real application.

서지기타정보

서지기타정보
청구기호 {DAE 96001
형태사항 xi, 139 p. : 삽화 ; 26 cm
언어 한국어
일반주기 저자명의 영문표기 : Byeong-Hee Chang
지도교수의 한글표기 : 장근식
지도교수의 영문표기 : Keun-Shik Chang
수록 잡지명: "Unsteady Adaptive Wall Models for Wind Tunnel Testing". AIAA Journal. AIAA, vol. 33, no. 8, pp. 1536-1538 (1995)
학위논문 학위논문(박사) - 한국과학기술원 : 항공우주공학과,
서지주기 참고문헌 : p. 59-66
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