Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques

Guilibaldo Tolentino; Miguel Toledo; Victor Zurita

Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques

Guilibaldo Tolentino, Miguel Toledo, Victor Zurita

Research output: Contribution to conference › Paper › peer-review

Abstract

In this paper are shown three techniques of flow visualization to analyze flows in axial compressor and turbine blades. An experimental analysis of the results is carried out in the LABINTHAP, employing the following techniques: a) smoke wire, b) tufts and c) oil film.

Original language	English
Pages	215-223
Number of pages	9
State	Published - 1995
Externally published	Yes
Event	Proceedings of the 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition - Hilton Head, SC, USA Duration: 13 Aug 1995 → 18 Aug 1995

Conference

Conference	Proceedings of the 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition
City	Hilton Head, SC, USA
Period	13/08/95 → 18/08/95

Cite this

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title = "Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques",

abstract = "In this paper are shown three techniques of flow visualization to analyze flows in axial compressor and turbine blades. An experimental analysis of the results is carried out in the LABINTHAP, employing the following techniques: a) smoke wire, b) tufts and c) oil film.",

author = "Guilibaldo Tolentino and Miguel Toledo and Victor Zurita",

year = "1995",

language = "Ingl{\'e}s",

pages = "215--223",

note = "Proceedings of the 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition ; Conference date: 13-08-1995 Through 18-08-1995",

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Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques. / Tolentino, Guilibaldo; Toledo, Miguel; Zurita, Victor.
1995. 215-223 Paper presented at Proceedings of the 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition, Hilton Head, SC, USA.

Research output: Contribution to conference › Paper › peer-review

TY - CONF

T1 - Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques

AU - Tolentino, Guilibaldo

AU - Toledo, Miguel

AU - Zurita, Victor

PY - 1995

Y1 - 1995

N2 - In this paper are shown three techniques of flow visualization to analyze flows in axial compressor and turbine blades. An experimental analysis of the results is carried out in the LABINTHAP, employing the following techniques: a) smoke wire, b) tufts and c) oil film.

AB - In this paper are shown three techniques of flow visualization to analyze flows in axial compressor and turbine blades. An experimental analysis of the results is carried out in the LABINTHAP, employing the following techniques: a) smoke wire, b) tufts and c) oil film.

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M3 - Artículo

AN - SCOPUS:0029431089

SP - 215

EP - 223

T2 - Proceedings of the 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition

Y2 - 13 August 1995 through 18 August 1995

ER -

Experimental study of boundary layer on a NACA 65-010 blade using some flow visualization techniques

Abstract

Conference

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