INTERFEROMETRIC TECHNIQUES AND DATA EVALUATION METHODS FOR THE UTIAS 10 cm multiplied by 18 cm HYPERVELOCITY SHOCK TUBE.

G. Ben-Dor; B. T. Whitten

INTERFEROMETRIC TECHNIQUES AND DATA EVALUATION METHODS FOR THE UTIAS 10 cm multiplied by 18 cm HYPERVELOCITY SHOCK TUBE.

G. Ben-Dor, B. T. Whitten

Department of Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

2 Scopus citations

Abstract

The experimental technique and instrumentation associated with the various measurements to study ionizing shock structures, flat-plate and side-wall boundary layers and nonstationary oblique shock wave diffractions over compression corners using the UTIAS 10 cm multiplied by 18 cm Hypervelocity Shock Tube are described. The maximum possible absolute and relative errors associated with these measurements are calculated for argon, krypton, oxygen and nitrogen which are usually used as test gases.

Original language	English
Journal	Toronto Univ Inst Aerosp Stud UTIAS Rep
Issue number	208
State	Published - 1 Jan 1979

ASJC Scopus subject areas

General Engineering

Cite this

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title = "INTERFEROMETRIC TECHNIQUES AND DATA EVALUATION METHODS FOR THE UTIAS 10 cm multiplied by 18 cm HYPERVELOCITY SHOCK TUBE.",

abstract = "The experimental technique and instrumentation associated with the various measurements to study ionizing shock structures, flat-plate and side-wall boundary layers and nonstationary oblique shock wave diffractions over compression corners using the UTIAS 10 cm multiplied by 18 cm Hypervelocity Shock Tube are described. The maximum possible absolute and relative errors associated with these measurements are calculated for argon, krypton, oxygen and nitrogen which are usually used as test gases.",

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N2 - The experimental technique and instrumentation associated with the various measurements to study ionizing shock structures, flat-plate and side-wall boundary layers and nonstationary oblique shock wave diffractions over compression corners using the UTIAS 10 cm multiplied by 18 cm Hypervelocity Shock Tube are described. The maximum possible absolute and relative errors associated with these measurements are calculated for argon, krypton, oxygen and nitrogen which are usually used as test gases.

AB - The experimental technique and instrumentation associated with the various measurements to study ionizing shock structures, flat-plate and side-wall boundary layers and nonstationary oblique shock wave diffractions over compression corners using the UTIAS 10 cm multiplied by 18 cm Hypervelocity Shock Tube are described. The maximum possible absolute and relative errors associated with these measurements are calculated for argon, krypton, oxygen and nitrogen which are usually used as test gases.

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JO - Toronto Univ Inst Aerosp Stud UTIAS Rep

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INTERFEROMETRIC TECHNIQUES AND DATA EVALUATION METHODS FOR THE UTIAS 10 cm multiplied by 18 cm HYPERVELOCITY SHOCK TUBE.

Abstract

ASJC Scopus subject areas

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