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CFD 해석 및 최적화 기법을 이용한 피토관 형상설계Design of Pitot-Tube Configuration Using CFD Analysis and Optimization Techniques

Other Titles
Design of Pitot-Tube Configuration Using CFD Analysis and Optimization Techniques
Authors
김도준천영성박영민최인호조태환명노신박찬우
Issue Date
2008
Publisher
대한기계학회
Keywords
Pitot-Tube(피토관); CFD(전산유체역학); RSM(반응면 기법); ADS(Air Data System; 대기자료계통)
Citation
대한기계학회논문집 B, v.32, no.5, pp 392 - 399
Pages
8
Indexed
SCOPUS
KCI
Journal Title
대한기계학회논문집 B
Volume
32
Number
5
Start Page
392
End Page
399
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/27986
ISSN
1226-4881
Abstract
Accurate measurement of speed and altitude of flying vehicles in air data system remains a critical technical issue. A highly reliable Pitot-static probe is required to obtain air data such as total pressure and static pressure. In this study, an analysis of the characteristics of flowfield around the Pitot-static probe was performed by using a Navier-Stokes CFD code. In addition, for the purpose of finding an optimal configuration, a technique based on the response surface method is applied to the problem with design parameters including shape of the nose section and cone angle. It is shown that the optimal configuration fulfills the MIL specification in wider range of high angles of attack.
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공학계열 > 기계항공우주공학부 > Journal Articles

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Myong, Rho Shin
대학원 (기계항공우주공학부)
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