Multi-hole pressure probes to air data system for subsonic small-scale air vehicles
A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi-hole pressure probe technique of measuring of a 3D flow to use in the ai...
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| creator | Shevchenko, A. M. Berezin, D. R. Puzirev, L. N. Tarasov, A. Z. Kharitonov, A. M. Shmakov, A. S. |
| description | A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi-hole pressure probe technique of measuring of a 3D flow to use in the air data system. Two multi-hole pressure probes with spherical and hemispherical head to air-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. The probes were calibrated in the wind tunnel, one of them is in-flight tested. |
| doi_str_mv | 10.1063/1.4963947 |
| format | Conference Proceeding |
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M. ; Berezin, D. R. ; Puzirev, L. N. ; Tarasov, A. Z. ; Kharitonov, A. M. ; Shmakov, A. S.</creator><contributor>Fomin, Vasily</contributor><creatorcontrib>Shevchenko, A. M. ; Berezin, D. R. ; Puzirev, L. N. ; Tarasov, A. Z. ; Kharitonov, A. M. ; Shmakov, A. S. ; Fomin, Vasily</creatorcontrib><description>A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi-hole pressure probe technique of measuring of a 3D flow to use in the air data system. Two multi-hole pressure probes with spherical and hemispherical head to air-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. 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S.</creatorcontrib><title>Multi-hole pressure probes to air data system for subsonic small-scale air vehicles</title><title>AIP Conference Proceedings</title><description>A brief review of research performed to develop multi-hole probes to measure of aerodynamic angles, dynamic head, and static pressure of a flying vehicle. The basis of these works is the application a well-known classical multi-hole pressure probe technique of measuring of a 3D flow to use in the air data system. Two multi-hole pressure probes with spherical and hemispherical head to air-data system for subsonic small-scale vehicles have been developed. A simple analytical probe model with separation of variables is proposed. The probes were calibrated in the wind tunnel, one of them is in-flight tested.</description><subject>Pressure head</subject><subject>Pressure sensors</subject><subject>Static pressure</subject><subject>Subsonic aircraft</subject><subject>Three dimensional flow</subject><subject>Vehicles</subject><subject>Wind tunnels</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2016</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kEFLAzEUhIMoWKsH_0HAm7A1L9lkN0cpWoWKBxW8hexulqZsmzUvW-i_d0sL3jy9OXwz8xhCboHNgCnxALNcK6Hz4oxMQErICgXqnEwY03nGc_F9Sa4Q14xxXRTlhHy8DV3y2Sp0jvbRIQ7xIELlkKZArY-0sclS3GNyG9qGSHGoMGx9TXFjuy7D2o7eA7hzK193Dq_JRWs7dDenOyVfz0-f85ds-b54nT8us15wkTJd2VY0qqjAqbJRouSKNay1snaVk22bKw6Ka9CSSwea1wVXtXANk7kWOSvFlNwdc8d_fwaHyazDELdjpeEwekFwgJG6P1JY-2STD1vTR7-xcW-AmcNoBsxptP_gXYh_oOmbVvwCh_ts1w</recordid><startdate>20161013</startdate><enddate>20161013</enddate><creator>Shevchenko, A. 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| fulltext | fulltext |
| identifier | ISSN: 0094-243X |
| ispartof | AIP Conference Proceedings, 2016, Vol.1770 (1) |
| issn | 0094-243X 1551-7616 |
| language | eng |
| recordid | cdi_proquest_journals_2121613211 |
| source | AIP Journals Complete |
| subjects | Pressure head Pressure sensors Static pressure Subsonic aircraft Three dimensional flow Vehicles Wind tunnels |
| title | Multi-hole pressure probes to air data system for subsonic small-scale air vehicles |
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