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Temperature Measurements by Laser-Induced Fluorescence Spectroscopy in Nonequilibrium High-Enthalpy Flow

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TLDR
In this paper, the rotational and translational temperature of NO molecules and O atoms in the freestream and behind a bow shock upstream of a blunt body is investigated by using the laser-induced fluorescence (LIF)diagnostictechnique.
Abstract
The e owe eld generated by the high-enthalpy arcjet facility L2K, simulating the stagnation conditions during shuttlereentry and mainly used for testing thermal protection materials, is investigated by using the laser-induced e uorescence (LIF)diagnostictechnique.FortheoperationconditionsoftheL2KfacilityofDLR,thee owconditions are dominated by nonequilibrium effects. In particular, translational and rotational temperatures are assumed to beinequilibrium,butlargedifferencesbetweenrotational,vibrational,and electronictemperatureoccur.Spatially resolved LIF is used to determine rotational and translational temperature of NO molecules and O atoms in the freestream and behind a bow shock upstream of a blunt body. The e ow is modeled numerically using a quasione-dimensional code and a full Navier ‐Stokes two-dimensional axisymmetric code. Good agreement is achieved between the experimental and numerical data in the freestream. The data are also compared with the coherent Stokes anti-Raman scattering measurements performed previously at the same e ow conditions in the same facility on the N2 molecules. Differences caused by the nonequilibrium aspects, in the freestream and across the shock layer, of N2, NO, and O components are evident, and the physical interpretation is discussed.

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Heat transfer—A review of 2005 literature

TL;DR: A review of the heat transfer literature published in 2005 can be found in this article, where the authors restrict themselves to papers published in English through a peer-review process, with selected translations from journals published in other languages.
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Experimental Verification of Heat-Flux Mitigation by Electromagnetic Fields in Partially-Ionized-Argon Flows

TL;DR: In this article, an experimental study on heat-flux mitigation within highenthalpy ionized-argon flows by application of an external magnetic-induction field was conducted using axially symmetric test models containing water-cooled magnet coils.
Journal ArticleDOI

Nitric-Oxide Planar Laser-Induced Fluorescence Measurements in the Hypersonic Materials Environmental Test System

TL;DR: In this paper, a planar laser-induced fluorescence of naturally occurring nitric oxide has been used to provide insight into baseline flow conditions of the Hypersonic Materials Environmental Test System 400kW arc-heated wind tunnel at NASA Langley Research Center via radial and axial velocity measurements and instantaneous flow-visualization images.
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Applied radiation physics techniques for diagnostic evaluation of the plasma wind and thermal protection system critical parameters in aerospace re-entry

TL;DR: In this paper, a review of the diagnostic methodologies used in hypersonic test facilities associated with the working principles, the development, the potential and the limitations of arc jet plasma wind tunnels for the evaluation of the aforementioned critical parameters is presented.
References
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Proceedings ArticleDOI

Thin-layer approximation and algebraic model for separated turbulent flows

B. Baldwin, +1 more
TL;DR: In this article, an algebraic turbulence model for two-and three-dimensional separated flows is specified that avoids the necessity for finding the edge of the boundary layer, and compared with experiment for an incident shock on a flat plate, separated flow over a compression corner, and transonic flow over an airfoil.
Journal ArticleDOI

Systematics of Vibrational Relaxation

TL;DR: In this article, a large number of data points for the vibrational relaxation time (pτv in atm sec) of simple systems have been logarithmically plotted vs (T°K)-⅓.
Journal ArticleDOI

Review of chemical-kinetic problems of future NASA missions, II: Mars entries

TL;DR: A number of chemical-kinetic problems related to phenomena occurring behind a shock wave surrounding an object flying in the earth atmosphere are discussed in this paper, including the nonequilibrium thermochemical relaxation phenomena behind a wave surrounding the flying object.
Proceedings ArticleDOI

On convergence of computation of chemically reacting flows

TL;DR: In this paper, the conservation equations governing chemical species and vibrational and electron energies are solved simultaneously with those for overall mass, momentum, and energy for a one-dimensional subsonic flow, through a constant-area duct, originating behind a normal shock wave, using an implicit time-marching technique.
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