Київський Міжнародний Університет Цивільної Авіації
Киевский международный университет гражданской авиации
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Application filed by Київський Міжнародний Університет Цивільної Авіації, Киевский международный университет гражданской авиацииfiledCriticalКиївський Міжнародний Університет Цивільної Авіації
Priority to UA98116308ApriorityCriticalpatent/UA31969A/en
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Measurement of air passing through air-jet engine flow rate in which one measures static pressure in minimal and maximal cross sections of measurement section and area of minimal cross section of that section. Measuring section is chosen in regular air inlet of engine, at that maximal cross section of measurement section corresponds to maximal cross section of channel of air inlet, and minimal – to minimal cross section of channel formed with inner surface of air inlet and cock of the engine, and air flow rate is determined through formula:
UA98116308A1998-11-301998-11-30Method for measurement of flow rate of air that goes through air-jet engine
UA31969A
(en)
Probe for measuring the speed or rate of flow of a flowing medium, in particular for air volume measurement, and pressure cell in particular for use with such a probe