Back to results
Bibliographic record · Consultation and access
Artículo de revista

Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration

Akhila Rupesh et al · Embry-Riddle Aeronautical University · 2020

Open access available
Quick overview. Review the resource’s basic details, then access the content using the main button. This page shows only the information needed to identify, cite, and open the work.
Serial publication

3D Printing Technology in Aerospace Industry – A Review

This serial publication contains 428 related contents.

Resource access

Open the content from the main option or choose another available source.

DOAJ DOAJ Articles
Entrar por DOAJ
Main access

Open access available

Recurso identificado como acceso abierto, sin confirmar automáticamente si es texto completo directo.
Open resource

Summary

Descripción general del contenido del recurso.

<p>It is very essential to predict the flow and its related parameters to understand real life fluid flow. The real-life fluid problems are studied with wind tunnels which gives very efficient results in practice. But in the case of wind tunnel studies flow angularities plays crucial role. Flow angularity determination includes measurement of static pressure, dynamic pressure and inflow angles. Flow prediction even hold a very strong hand in design process. Designing and testing being the foundation of any process industry, flow measurements and its related parameters have to be well evaluated. In such cases, wind tunnels play important role and the researchers are usually dependent on wind tunnels to carry out experiments at different Mach numbers to obtain experimental results. It is mandatory to check the flow parameters and maturity rates including turbulence, flow angularity, strain, velocity, temperature and density distribution at the test section before testing a model. The flow field and degree of maturity within the test section can be analysed with any instrument that will provide a flow field data diagram of test parts. In this paper, the performance evaluation and truthiness of five-hole five probe flow analyser is being evaluated computationally and experimentally at various Mach Numbers.</p>

How to cite

Elegí el formato que necesitás y copiá la referencia al portapapeles.

APA 7

al, A. R. E. (2020). Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration. https://doi.org/10.15394/ijaaa.2020.1523

MLA

al, Akhila Rupesh et. "Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration." 2020. https://doi.org/10.15394/ijaaa.2020.1523.

Chicago

al, Akhila Rupesh et. 2020. "Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration.". https://doi.org/10.15394/ijaaa.2020.1523.

Harvard

al, A. R. E. 2020, Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration, Embry-Riddle Aeronautical University, available at: https://doi.org/10.15394/ijaaa.2020.1523 [Accessed 8 Aug. 2026].

Share and print

Save the record, copy its permanent link, or print it as a PDF.

Export reference

You can export the record in common formats for use in a reference manager.

Resource details

Bibliographic information to help confirm that this is the correct material.

Title
Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration
Author / contributors
Akhila Rupesh et al
Publisher
Embry-Riddle Aeronautical University
Publication year
2020
ISSN
2374-6793
ISSN
2374-6793
Language
English

Subjects

Explore related resources through these subjects.

Copied