SU1828695A3 - Device for measuring pitot and static pressure at aerodynamic model flow passage outlet - Google Patents

Device for measuring pitot and static pressure at aerodynamic model flow passage outlet

Info

Publication number
SU1828695A3
SU1828695A3 SU4946898/23A SU4946898A SU1828695A3 SU 1828695 A3 SU1828695 A3 SU 1828695A3 SU 4946898/23 A SU4946898/23 A SU 4946898/23A SU 4946898 A SU4946898 A SU 4946898A SU 1828695 A3 SU1828695 A3 SU 1828695A3
Authority
SU
USSR - Soviet Union
Prior art keywords
static pressure
flow passage
passage outlet
nozzle
model flow
Prior art date
Application number
SU4946898/23A
Other languages
Russian (ru)
Inventor
Т.М. Сахненко
Н.А. Юденков
Original Assignee
Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского filed Critical Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority to SU4946898/23A priority Critical patent/SU1828695A3/en
Application granted granted Critical
Publication of SU1828695A3 publication Critical patent/SU1828695A3/en

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Landscapes

  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Measuring Arrangements Characterized By The Use Of Fluids (AREA)

Abstract

FIELD: aerodynamics. SUBSTANCE: device has nozzle 1 and ridge 2 with Pitot tube and static pressure pick-up. Pitot tubes 4 are located at distance of a-(1-2)d from exit section of nozzle 1 and at distance of Δ=(0,5-1,0)d, from nozzle wall. Static pressure pick-ups are located in center of space between pylons; total area of blocking of nozzle 1 is equal to F/F. EFFECT: enhanced accuracy of measurement. 6 dwg
SU4946898/23A 1991-06-18 1991-06-18 Device for measuring pitot and static pressure at aerodynamic model flow passage outlet SU1828695A3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4946898/23A SU1828695A3 (en) 1991-06-18 1991-06-18 Device for measuring pitot and static pressure at aerodynamic model flow passage outlet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4946898/23A SU1828695A3 (en) 1991-06-18 1991-06-18 Device for measuring pitot and static pressure at aerodynamic model flow passage outlet

Publications (1)

Publication Number Publication Date
SU1828695A3 true SU1828695A3 (en) 1996-02-20

Family

ID=60541326

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4946898/23A SU1828695A3 (en) 1991-06-18 1991-06-18 Device for measuring pitot and static pressure at aerodynamic model flow passage outlet

Country Status (1)

Country Link
SU (1) SU1828695A3 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108896121A (en) * 2018-06-08 2018-11-27 华北电力大学 A kind of axial flow blower flow measurement device based on cross probe
CN113358320A (en) * 2021-08-10 2021-09-07 中国空气动力研究与发展中心高速空气动力研究所 Method for measuring force of interference of jet flow of upstream air for high-speed wind tunnel
RU222943U1 (en) * 2023-10-27 2024-01-24 Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") Device for measuring total, dynamic and static pressure of aerodynamic flow

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108896121A (en) * 2018-06-08 2018-11-27 华北电力大学 A kind of axial flow blower flow measurement device based on cross probe
CN113358320A (en) * 2021-08-10 2021-09-07 中国空气动力研究与发展中心高速空气动力研究所 Method for measuring force of interference of jet flow of upstream air for high-speed wind tunnel
RU222943U1 (en) * 2023-10-27 2024-01-24 Федеральное автономное учреждение "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФАУ "ЦАГИ") Device for measuring total, dynamic and static pressure of aerodynamic flow

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