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Double Probe Recovery Temperature Anemometry

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00347454" target="_blank" >RIV/68407700:21220/21:00347454 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.1016/j.tsep.2021.100875" target="_blank" >https://doi.org/10.1016/j.tsep.2021.100875</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.tsep.2021.100875" target="_blank" >10.1016/j.tsep.2021.100875</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Double Probe Recovery Temperature Anemometry

  • Original language description

    It is known that the temperature rendered by temperature probes positioned within an airflow depends on the thermodynamic temperature, the external flow velocity, the specific heat of the fluid, and the recovery factor of the probe. The said dependence is essential for the external velocity measurement by the method of Recovery Temperature Anemometry (RTA). Even if both the recovery factor of the probe and isobaric heat capacity are known, one also has to know the external flow velocity for the evaluation of the thermodynamic temperature or, the thermodynamic temperature for the evaluation of the flow velocity. This means there are two unknown properties in real-time measurements – thermodynamic temperature and velocity. This article deals with the possible solution to the mentioned problem. By the use of two probes with different recovery factors, the need for knowing the thermodynamic temperature is eliminated, so that a combination of two temperature probes with different recovery factors can be used for the velocity measurement.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database

  • CEP classification

  • OECD FORD branch

    20303 - Thermodynamics

Result continuities

  • Project

    <a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2021

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    Thermal Science and Engineering Progress

  • ISSN

    2451-9049

  • e-ISSN

    2451-9049

  • Volume of the periodical

  • Issue of the periodical within the volume

    February

  • Country of publishing house

    NL - THE KINGDOM OF THE NETHERLANDS

  • Number of pages

    18

  • Pages from-to

  • UT code for WoS article

    000677531700006

  • EID of the result in the Scopus database

    2-s2.0-85102078421