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Comparison of mathematical simulation results and experimental research of PVD-K3-1 air pressure probe
- Authors: Moiseev V.N.1, Dubinina M.M.1, Pavlovsky A.A.1, Sorokin M.Y.1
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Affiliations:
- JSC «Ulyanovsk instrument manufacturing design bureau»
- Issue: Vol 11, No 5-2 (2012): Special Issue
- Pages: 229-235
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2321
- DOI: https://doi.org/10.18287/2541-7533-2012-0-5-2(36)-229-235
- ID: 2321
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Abstract
The paper presents the test results and mathematical modeling data of air pressure probes and gives justification of using mathematical modeling in further design of similar air pressure probes, as well as provides estimate of applicability of OpenFOAM program for modeling air pressure probe. The paper also gives impact of air stream wash on measurement error of air pressure.
About the authors
V. N. Moiseev
JSC «Ulyanovsk instrument manufacturing design bureau»
Author for correspondence.
Email: v.n.moiseev@mail.ru
Engineer of Department
Russian FederationM. M. Dubinina
JSC «Ulyanovsk instrument manufacturing design bureau»
Email: masha_dubinina.73@mail.ru
Engineer of Department
Russian FederationA. A. Pavlovsky
JSC «Ulyanovsk instrument manufacturing design bureau»
Email: rto@ukbp.ru
Head of Crew
Russian FederationM. Y. Sorokin
JSC «Ulyanovsk instrument manufacturing design bureau»
Email: rto@ukbp.ru
Candidate of Engineering Sciences
Head of Department
Russian FederationReferences
- NASA Technical Report 1303 “Windtunnel investigation of a number of totalpressure tubes at high angles of attack subsonic, transonic and supersonic speeds” by William Gracey, 1956.
- Клюев, Г.И. Измерители аэродинамических параметров летательных аппаратов: учебное пособие [Текст] / Г.И. Клюев, Н.Н. Макаров, В.М. Солдаткин, И.П. Ефимов; под ред. В.А. Мишина. – Ульяновск: УлГТУ, 2005. – 509 с.
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