Impingement of axisymmetric under-expanded sonic jets on a flat plate

Byung Gi Kim; Man Sun Yu; Hyung Hee Cho; Ki Young Hwang; Joo Chan Bae

doi:10.1115/IMECE2002-33612

Impingement of axisymmetric under-expanded sonic jets on a flat plate

Byung Gi Kim, Man Sun Yu, Hyung Hee Cho, Ki Young Hwang, Joo Chan Bae

Department of Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

An experimental investigation has been carried out to examine heat transfer characteristics of an axisymmetric, under-expanded, and sonic jet impinging on a flat plate. Distributions of recovery factor and the surface pressure on the flat plate have been obtained in detail. The ratio of nozzle exit pressure to the ambient pressure, i.e., under-expansion ratio ranges from 1.5 to 3.5 and the nozzle-to-plate distance is tested from 0.5 to 20.0 nozzle exit diameters. It has been found that the recovery factor varies from 0.35 up to over 1.25 depending on both parameters of interest within the present experimental range.

Original language	English
Title of host publication	Heat Transfer
Publisher	American Society of Mechanical Engineers (ASME)
Pages	123-130
Number of pages	8
ISBN (Print)	0791836355, 9780791836354
DOIs	https://doi.org/10.1115/IMECE2002-33612
Publication status	Published - 2002 Jan 1
Event	ASME 2002 International Mechanical Engineering Congress and Exposition, IMECE2002 - New Orleans, LA, United States Duration: 2002 Nov 17 → 2002 Nov 22

Publication series

Name	ASME International Mechanical Engineering Congress and Exposition, Proceedings
Volume	4

Other

Other	ASME 2002 International Mechanical Engineering Congress and Exposition, IMECE2002
Country	United States
City	New Orleans, LA
Period	02/11/17 → 02/11/22

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All Science Journal Classification (ASJC) codes

Mechanical Engineering

Cite this

Kim, B. G., Yu, M. S., Cho, H. H., Hwang, K. Y., & Bae, J. C. (2002). Impingement of axisymmetric under-expanded sonic jets on a flat plate. In Heat Transfer (pp. 123-130). (ASME International Mechanical Engineering Congress and Exposition, Proceedings; Vol. 4). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/IMECE2002-33612

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abstract = "An experimental investigation has been carried out to examine heat transfer characteristics of an axisymmetric, under-expanded, and sonic jet impinging on a flat plate. Distributions of recovery factor and the surface pressure on the flat plate have been obtained in detail. The ratio of nozzle exit pressure to the ambient pressure, i.e., under-expansion ratio ranges from 1.5 to 3.5 and the nozzle-to-plate distance is tested from 0.5 to 20.0 nozzle exit diameters. It has been found that the recovery factor varies from 0.35 up to over 1.25 depending on both parameters of interest within the present experimental range.",

author = "Kim, {Byung Gi} and Yu, {Man Sun} and Cho, {Hyung Hee} and Hwang, {Ki Young} and Bae, {Joo Chan}",

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Kim, BG, Yu, MS, Cho, HH, Hwang, KY & Bae, JC 2002, Impingement of axisymmetric under-expanded sonic jets on a flat plate. in Heat Transfer. ASME International Mechanical Engineering Congress and Exposition, Proceedings, vol. 4, American Society of Mechanical Engineers (ASME), pp. 123-130, ASME 2002 International Mechanical Engineering Congress and Exposition, IMECE2002, New Orleans, LA, United States, 02/11/17. https://doi.org/10.1115/IMECE2002-33612

Impingement of axisymmetric under-expanded sonic jets on a flat plate. / Kim, Byung Gi; Yu, Man Sun; Cho, Hyung Hee; Hwang, Ki Young; Bae, Joo Chan.

Heat Transfer. American Society of Mechanical Engineers (ASME), 2002. p. 123-130 (ASME International Mechanical Engineering Congress and Exposition, Proceedings; Vol. 4).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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AB - An experimental investigation has been carried out to examine heat transfer characteristics of an axisymmetric, under-expanded, and sonic jet impinging on a flat plate. Distributions of recovery factor and the surface pressure on the flat plate have been obtained in detail. The ratio of nozzle exit pressure to the ambient pressure, i.e., under-expansion ratio ranges from 1.5 to 3.5 and the nozzle-to-plate distance is tested from 0.5 to 20.0 nozzle exit diameters. It has been found that the recovery factor varies from 0.35 up to over 1.25 depending on both parameters of interest within the present experimental range.

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Access to Document

10.1115/IMECE2002-33612