Impact of sensor housing geometries on transient stagnation pressure measurements in impulse facilities-Reference-Cited by-同舟云学术

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Impact of sensor housing geometries on transient stagnation pressure measurements in impulse facilities

Published:2019-12 Issue: Volume:109 Page:109851
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Wang Zhaoguang,Giglmaier Marcus,Hopfes Thomas,Köglmeier Lea,Adams Nikolaus A.

Funder

European Research Council

China Scholarship Council

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference18 articles.

1. Rex Klopfenstein Jr., Air velocity and flow measurement using a Pitot tube, ISA transactions 37, no. 4 (1998) 257–263.

2. The Ludwieg pressure-tube supersonic wind tunnel;Cable;Aeronaut. Quart.,1963

3. Aeronautical Research Council, Bow-shock establishment and stagnation-point pressure measurements for a blunt-nosed body at supersonic speeds, HM Stationery Office, 1965.

4. J.D. Anderson, Modern Compressible Flow with Historical Perspective, 2003.

5. Richard Gilman Folsom, Review of the Pitot tube, 1955.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental Investigation of a Line-Cavity System Equipped with Fiber-Optic Differential Pressure Sensors in a Shock Tube;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2021

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