Velocity and NO-Lifetime Measurements in an Unseeded Hypersonic Air Flow

Author:

Matos Pedro A. de S.1,Barreta Luiz G.2,Martins Cristiane A.3

Affiliation:

1. Energy, Propulsion and Combustion Laboratory, Department of Propulsion, Aeronautics Institute of Technology, São José dos Campos 12228-900, São Paulo, Brazil; Laboratory of Aerothermodynamics and Hypersonics, Institute for Advanced Studies, São José dos Campos 12228-001, São Paulo, Brazil e-mail:

2. Laboratory of Aerothermodynamics and Hypersonics, Institute for Advanced Studies, São José dos Campos 12228-001, São Paulo, Brazil; Energy, Propulsion and Combustion Laboratory, Department of Propulsion, Aeronautics Institute of Technology, São José dos Campos 12228-900, São Paulo, Brazil e-mail:

3. Energy, Propulsion and Combustion Laboratory, Department of Propulsion, Aeronautics Institute of Technology, São José dos Campos 12228-900, São Paulo, Brazil e-mail:

Abstract

A laser-induced fluorescence (LIF)-based nitric-oxide flow-tagging technique was applied to measure both velocity and NO lifetime in a hypersonic shock tunnel from two experimental test runs. The results were supported by an analytical profile proposed in this paper that provides a way to correct velocity measurements under unknown systematic error sources. This procedure provided velocities with discrepancies lower than 3% for a total of five measurements, and lower than 2% when compared with that obtained from a linear fit. Additionally, the comparison between the proposed and experimental profiles allowed us to obtain the fluorescence NO lifetime from only one image.

Funder

Financiadora de Estudos e Projetos

Publisher

ASME International

Subject

Mechanical Engineering

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