Convective heat-transfer rate and surface pressure distribution over a cone model at hypersonic speeds-Reference-Cited by-同舟云学术

Convective heat-transfer rate and surface pressure distribution over a cone model at hypersonic speeds

Published:2018-10-11 Issue:10 Volume:233 Page:3649-3664
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Saiprakash M¹^ORCID,SenthilKumar C¹,Balu G²,Shanmugam V²,Rampratap Singh Prakash²,sunil G Kadam²

Affiliation:

1. Department of Aerospace Engineering, Anna University, Chennai, India

2. Directorate of Aerodynamics, Defence Research & Development Laboratory, Hyderabad, India

Abstract

In this article, experiments are carried out in a hypersonic shock tunnel with helium as driver gas and air as the test gas to obtain the convective heating rate and surface pressure distribution on a cone model placed at hypersonic speed. Test is performed in hypersonic shock tunnel for a flow Mach number of 6.5 at two different angles of attack, 0° and 5°. The sputtered thin film platinum sensors are used to measure the heat flux on a cone model. The measured heat-transfer rate compares well with theoretically estimated values using reference enthalpy method and computational fluid dynamics (CFD) simulation. The measured surface pressure compares well with CFD.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410018804691

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1. Heat Transfer Measurements over Large Angle Blunt Cones Entering Martian Atmosphere

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4. Performance evaluation of coaxial thermocouple against platinum thin film gauge for heat flux measurement in shock tunnel

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