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순차 컨벡스 프로그래밍 기반 무인기 설계 형상의 성능 분석
고효상,최한림,장종윤,김준,유구현,Ko, Hyo-Sang,Choi, Hanlim,Jang, Jong-Youn,Kim, Joon,Ryu, Gu-Hyun 한국항공우주학회 2022 韓國航空宇宙學會誌 Vol.50 No.11
Sequential convex programming based performance analysis of the designed UAV is performed. The nonlinear optimization problems generated by aerodynamics are approximated to socond order program by discretization and convexification. To improve the performance of the algorithm, the solution of the relaxed problem is used as the initial trajectory. Dive trajectory optimization problem is analyzed through iterative solution procedure of approximated problem. Finally, the maximum final velocity according to the performance of the actuator model was compared.
스크램제트 추진 시스템 모델링을 통한 유동 특성 산출 알고리즘에 대한 연구
고효상(Hyosang Ko),최한림(Hanlim Choi) 한국추진공학회 2019 한국추진공학회 학술대회논문집 Vol.2019 No.11
공기 흡입식 극초음속 비행체인 스크램제트의 모델링과 그에 대한 유동 특성 산출 알고리즘에 대해 연구했다. 설계된 모델에 생기는 충격파 형상과 연소 현상을 가정한 대기 조건과 연료에 대해 분석하였고, 이를 통해 다양한 비행조건에서 동체에 발생하는 힘과 모멘트를 분석하였다. 분석한 모델에 대해서 비행 정보 획득을 위한 알고리즘에 대해 연구했으며 다양한 비행조건과 알고리즘을 통해 추정한 비행 정보를 비교해 보았다. The modelling of air-breathing hypersonic vehicle and it’s air data acquisition algorithm were studied. Under various flight conditions, force and moment were calculated through the analysis of shock wave shapes and combustion phenomenon. In addition, the algorithm for estimating air data was presented and the result of it was compared with real air data for various flight conditions.
스크램제트 추진 시스템의 비행 제어를 통한 연소기의 추력 분석
고효상(Hyosang Ko),양재훈(Jaehoon Yang),여재익(Jai ick Yoh),최한림(Hanlim Choi) 한국추진공학회 2021 한국추진공학회지 Vol.25 No.1
The PID controller with fin angle and thrust as control input was designed based on the aerodynamic data of scramjet system. Flight simulation following a given trajectory which strike the target point after climb and cruise with constant dynamic pressure was conducted. After that, the required thrust for the climb and cruise was calculated and the required fuel flow rate for the hydrogen fuel dual mode scramjet combustor was analyzed. The combustor analysis of this study which conducted on integrated model of independently developed inlet, combustor, nozzles and external aerodynamic models, laying the foundation for the integrated design of the air breathing hypersonic system.
Primary hepatic choriocarcinoma in a female patient
Makhmud Malikov,Eun Shin(신은),Jai Young Cho(조재영),Ho-Seong Han(한호성),You-Seok Yoon(윤유석),Young Rok Choi(최영록),Jae Yool Jang(장재율),Hanlim Choi(최한림),Jae Seong Jang(장재성),Seong Uk Kwon(권성욱),Haeryoung Kim(김혜령) 대한종양외과학회 2015 Korean Journal of Clinical Oncology Vol.11 No.1
정상 면역 환자에서 췌장암으로 오인된 원발성 췌장 칸디다증
김충현 ( Chung Hyoun Kim ),이현민 ( Hyeonmin Lee ),우창곡 ( Chang Gok Woo ),한정호 ( Joung-ho Han ),최한림 ( Hanlim Choi ),박선미 ( Seon Mee Park ) 대한소화기학회 2021 대한소화기학회지 Vol.77 No.1
Pancreatic candidiasis can develop in patients with acute pancreatitis, compromised immune responses, or iatrogenic intervention. This paper reports a case of pancreatic candidiasis presenting as a solid pancreatic mass in a patient without the risk factors. A previously healthy 37-year-old man visited the emergency department with left flank pain. Abdominal CT revealed a 5 cm, irregular heterogeneous enhancing mass accompanied by a left adrenal mass. Positron emission tomography-computed tomography and endoscopic ultrasound-guided fine-needle aspiration (EUS-FNA) could not discriminate pancreatic cancer from infectious disease. A laparoscopic exploration was performed for an accurate diagnosis. After distal pancreatectomy with splenectomy and left adrenalectomy, pancreatic candidiasis and adrenal cortical adenoma were diagnosed based on the pathology findings. His condition improved after the treatment with fluconazole. This paper reports a case of primary pancreatic candidiasis mimicking pancreatic cancer in an immunocompetent patient with a review of the relevant literature. (Korean J Gastroenterol 2021;77:45-49)