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<div>Laser-absorption spectroscopy (LAS) is widely used for providing non-intrusive and quantitative measurements of gas properties (such as temperature and absorbing species mole fraction) in combustion environments. However, challenges may arise from the line-of-sight nature of LAS diagnostics, which can limit their spatial resolution. Further, time-resolution of such techniques as scanned direct-absorption or wavelength-modulation spectroscopy is limited by the scanning speed of the laser and the optical bandwidth is often limited by a combination of a laser's intrinsic tunability and its scanning speed. The work presented in this dissertation investigated how recent advancements in mid-IR camera technology and lasers can be leveraged to expand the spatial, temporal, and spectral measurement capabilities of LAS diagnostics. Novel laser-absorption imaging and ultrafast laser-absorption spectroscopy diagnostics are presented in this dissertation. In addition, the high-pressure combustion chamber (HPCC) and high-pressure shock tube (HPST) were designed and built to enable the study of, among others, energetic material combustion, spectroscopy, non-equilibrium and chemistry using optical diagnostics.<br></div><div><br></div>

Les diagnostics lasers ont prouvé leur potentiel pour l'analyse des écoulements et des phénomènes de combustion par la mesure de champs de vitesses, de concentration d'espèces et de température. La diffusion Raman spontanée (DRS) est une des rares méthodes permettant de mesurer la température et la concentration de manière in-situ avec la possibilité de sonder plusieurs espèces simultanément. L'analyse des flammes turbulentes par DRS est difficile en raison de la nécessité de mesures mono-coup avec de fortes résolutions spatiales et temporelles et de la présence de lumière parasite. L'originalité de notre nouveau dispositif de mesure réside dans l'utilisation d'un obturateur électro-optique à base de cellule de Pockels (OCP), permettant d'éliminer les lumières non polarisées de fond de flamme, compatible avec une mesure 1D. Une réduction significative de l'émission de flamme et une amélioration du rapport signal sur bruit des espèces Raman actives ont été obtenues. La capacité de la DRS en tant que méthode de thermométrie mono-coup a été testée avec succès dans le cas d'une flamme de prémélange et de diffusion laminaire fuligineuse. L'écart relatif entre les températures moyennes mesurées dans les gaz brûlés et celles données par la modélisation de flamme est inférieur à 1 %. L'analyse de la thermométrie Raman à basse température a montré qu'une meilleure précision était obtenue avec la modélisation de 02 comparée à celle N2. Par la suite, le potentiel de la DRS à fournir des mesures simultanées de concentrations instantanées de N2, 02 et CO dans les flammes a été validé. Une évaluation des performances de différents détecteurs CCD accompagnés de l'OCP a également été réalisée. Les résultats obtenus avec la BI-CCD et la BI-EMCCD pour la température, le gradient de température et la forte densité sont en bon accord avec les calculs laminaires 1D de flamme adiabatique fournis par COSILAB. La BI-EMCCD a montré qu'elle est le détecteur le plus sensible pour la détection des espèces à faibles concentrations comme le CO. Enfin, des mesures par DRS ont été obtenues dans une flamme-jet de diffusion turbulente, en présence des suies illustrant le potentiel de cette technique pour construire une base de données importante pour la modélisation numérique des flammes / Laser diagnostics have been proven to be an indispensable tool to analyze the flow and combustion phenomena by allowing non-intrusive measurements of the velocity field, concentration and temperature. Spontaneous Raman Scattering (SRS) is one of the few methods providing simultaneously in-situ temperature and multi-species concentrations. Measurement in turbulent flames by SRS is still challenging due to the emission background and the requirement of single-shot measurements with high spatial and temporal resolutions. The originality of the present approach consists in use of a large aperture Pockels cell based electro-optical shutter (PCS), that allows removing unpolarised background flame emission and compatible with a 1D measurement. A significant reduction of flame emission was observed and consequently signal to noise ratio was enhanced. The ability of SRS in terms of thermometric single-shot method was demonstrated successfully in premixed laminar flames and sooty laminar diffusion flames. The measured temperature in burnt gases and those calculated by adiabatic flame modelling was within 1 %. Thermometric Raman analysis for low temperatures demonstrates the reliability of measurements, with a better accuracy for 02 compared to N2. Subsequently, the ability of SRS technique to simultaneously measure instantaneous concentrations of N2, 02 and CO was demonstrated. The ability to measure single-shot scalar values accurately is assessed by comparing different CCD detectors with the PCS. The results obtained from the BI-CCD and the BI-EMCCD concerning temperature, temperature gradient and high density were in good agreement with the COSILAB calculation for 1D laminar adiabatic flame. The BI-EMCCD observed to be the most sensitive in detecting low concentration elements like CO. Finally, SRS technique was applied to a turbulent sooting jet flame, illustrating the potentiel of this technique to build an important database for flame modelling

Combustion phenomena are complex in theory and expensive to test, analysis techniques<br>provide handles with which we may describe them. Just as simultaneous experimental tech-<br>niques provide complementary descriptions of flame behavior, one might assume that no<br>analysis technique for any kind of flame measurement would cover the full description of<br>the flame. To this end, the search continues for complementary descriptions of engineering<br>flames that capture enough information for the engine designer to make informed decisions.<br>The kinds of flames I have encountered are high pressure transverse jet flames issuing into a<br>vitiated crossflow which is itself generated from combustion of a gaseous fuel and oxidizer.<br>Summarizing the behavior of these flames has required my understanding of experimen-<br>tal techniques such as Planar Laser Induced Fluorescence of a reaction intermediate -OH,<br>Particle Image Velocimetry of a passive tracer in the flame and OH * chemiluminescence of<br>another reaction intermediate. The analysis tools applied to these measurements must reveal<br>as much information as is laden in these measurements.<br>In this work I have also used wavelet optical flow to track flow features in the visualization<br>of combustion intermediates using OH * chemiluminescence. There are many limitations to<br>the application of this technique to engineering flames especially due to the interpretation<br>of the data as a 2-D motion field in 3-D world. The interpretation of such motion fields<br>as generated by scalar fields is one subject matter discussed in this dissertation. Some<br>inferences from the topology of the ensuing velocity field has provided insight to the behavior<br>of reacting turbulent flows which appear attached to an injector in the mean field. It gives<br>some understanding to the robustness of the attachment mechanism when such flames are<br>located near walls.

Τα τελευταία χρόνια, η φασματοσκοπία πλάσματος επαγόμενο από λέιζερ (LIBS) έχει προσελκύσει μεγάλο ερευνητικό ενδιαφέρον καθώς αποτελεί μία πειραματικά απλή και αποτελεσματική τεχνική, η οποία παρέχει τη δυνατότητα λήψης μετρήσεων για απευθείας ποιοτική και ποσοτική στοιχειακή ανάλυση. Η τεχνική LIBS στηρίζεται στη δημιουργία σπινθήρα/πλάσματος μέσω ισχυρά εστιασμένης δέσμης λέιζερ στην επιφάνεια ή στο εσωτερικό του δείγματος, στην ακόλουθη διέγερση και ατομοποίηση των στοιχείων του στόχου και στην τελική καταγραφή και φασματοσκοπική ανάλυση της εκπεμπόμενης ακτινοβολίας του πλάσματος. Λόγω των πολλών πλεονεκτημάτων που συγκεντρώνει η τεχνική, το LIBS έχει προταθεί για πληθώρα πρακτικών, τεχνικών και τεχνολογικών εφαρμογών σε ένα ευρύ φάσμα ερευνητικών πεδίων. Από την άλλη μεριά, στον τομέα της καύσης, η ποσότητα καυσίμου σε ένα εύφλεκτο μίγμα είναι αντικείμενο μείζονος σημασίας καθώς επηρεάζει σημαντικά την απόδοση των χημικών διεργασιών και την παραγωγή και εκπομπή ρύπων. Επομένως, δημιουργείται η ανάγκη ανάπτυξης μίας γρήγορης και μη παρεμβατικής διαγνωστικής τεχνικής για τη μέτρηση της περιεκτικότητας του καυσίμου τοπικά στη φλόγα με καλή τόσο χωρική όσο και χρονική ανάλυση. Στα πλαίσια της παρούσας διδακτορικής διατριβής, η τεχνική LIBS η οποία συγκεντρώνει όλα αυτά τα πλεονεκτήματα χρησιμοποιήθηκε για αυτό το σκοπό. Κατά τη διάρκεια των πειραμάτων, χρησιμοποιήθηκαν πηγές λέιζερ διάρκειας παλμών ns και fs, ενώ τα συστήματα καύσης που μελετήθηκαν ήταν φλόγες υδρογονανθράκων-αέρα, στρωτής και τυρβώδους ροής, απλής και συνθετότερης γεωμετρίας. Από τα LIBS φάσματα φλογών διαφορετικής σύστασης, προέκυψε λοιπόν ότι υπάρχει μία ισχυρή εξάρτηση μεταξύ των εντάσεων διαφόρων φασματικών γραμμών με το λόγο ισοδυναμίας. Επομένως, μέσω της συσχέτισης αυτής μπορεί να επιτευχθεί με μεγάλη ακρίβεια τόσο η μέτρηση της περιεκτικότητα σε καύσιμο φλογών άγνωστης σύστασης όπως επίσης και η μέτρηση της κατανομής του καυσίμου τοπικά μέσα σε όλη την έκταση της φλόγας παρέχοντας σημαντικές πληροφορίες για την δομή της. Τέλος, εφαρμόστηκε μία παραπλήσια διαγνωστική τεχνική, κατά την οποία η διηλεκτρική κατάρρευση του μέσου ήταν αποτέλεσμα ενός ηλεκτρικού σπινθήρα: electrical Spark Induced Breakdown Spectroscopy (SIBS) όπου και πραγματοποιήθηκε η συγκριτική μελέτη της ακτινοβολίας του πλάσματος επαγόμενο μέσω οπτικής και ηλεκτρικής διέγερσης. / Laser induced breakdown spectroscopy (LIBS) has attracted a lot of scientific interest during the last two decades as it is generally considered to be an experimentally simple and efficient laser-based technique which can perform real-time, qualitative and quantitative elemental analysis. The basic idea of LIBS is the creation of spark/plasma through tight focusing of a laser beam on the surface or into a sample, the subsequent excitation and atomization of the species of the sample at the location where the spark is formed and the final detection and spectroscopic analysis of the emitted radiation from the decaying plasma. Seeing the numerous advantages holding the technique, LIBS has been proposed for many practical, technical and technological applications in various scientific areas. On the other hand, in the field of combustion, the proportion of fuel in a combustible mixture is of great importance as it strongly affects the efficiency of the chemical processes and the production of soot emissions. Therefore, there is a continuously increasing need for the development of a rapid and non-perturbative diagnostic technique for the determination of the fuel content locally in the flame structure with good spatial and temporal resolution. Ιn the present dissertation, LIBS technique which offers such advantages has been applied for combustion diagnostics purposes. During the experiments, laser systems with pulse duration in the scale of ns and fs have been applied as excitation sources, while the combustible mixtures under investigation were hydrocarbon-air flames, of laminar and turbulent flow with simple and more complicated structures. From the LIBS spectra in flames of different compositions, it was exhibited that there is a strong dependence of the intensities of various spectral lines on the equivalence ratio, which demonstrates that the precise determination of the amount of fuel can be performed. Also based on this correlation, the determination of the equivalence ratio locally everywhere within the flame can be achieved giving useful information about its structure. Finally, a similar diagnostic technique has been employed. The dielectric breakdown is held using a spark generator and the technique is called electrical Spark Induced Breakdown Spectroscopy (SIBS). The emitted light of the two plasmas induced by optical and electrical excitation was collected and a comparative study was performed.

<p dir="ltr">The objective of this research is to advance the development and application of laser diagnostics in gas phase medium, which ranges from atmospheric non-reacting flows to turbulent reacting flows in high-pressure, high-temperature environments. Laser diagnostic techniques are powerful tools for non-intrusive and in-situ measurements of important chemical parameters, such as temperature, pressure, and species mole fractions, in harsh environments. These measurements significantly advance the knowledge across various research disciplines, such as combustion dynamics, chemical kinetics, and molecular spectroscopy. In this thesis, detailed theoretical models and experimental analysis are presented for three different techniques: 1. Chirped-probe-pulse femtosecond coherent anti-Stokes Raman scattering (CPP fs CARS); 2. Two-color polarization spectroscopy (TCPS); 3. Ultrafast-laser-absorption-spectroscopy (ULAS). The first chapter provides a brief survey of laser diagnostics, including both linear and nonlinear methods. The motivations behind the three studies covered in this dissertation are also discussed. </p><p dir="ltr">In the second chapter, single-shot CPP fs CARS thermometry is developed for the hydrogen molecule at 5 kHz. The results are divided into two parts. The first part concentrates on the development of H₂ CPP fs CARS thermometry for high-pressure and high-temperature conditions. The second part demonstrates the application of H₂ CPP fs CARS in a model rocket combustor at pressures up to 70 bar. In the first part, H₂ fs CARS thermometry was performed in Hencken burner flames up to 2300 K, as well as in a heated gas-cell at temperatures up to 1000 K. It was observed that the H₂ fs CARS spectra are highly sensitive to the pump and Stokes chirp. Chirp typically originates from optical components such as windows and polarizers. As a result, the pump delay is modeled to provide a shift to the Raman excitation efficiency curve. With the updated theoretical model, excellent agreement was found between the simulated and experimental spectra. The averaged error and precision are 2.8% and 2.3%, respectively. In addition, the spectral phase and pump delay determined from the experimental spectra closely align with the theoretical predictions. It is also found that pressure does not have significant effects on the H₂ fs CARS spectra up to 50 bar at 1000 K. The collision model provides excellent agreement with the experiment. This allows the use of low-pressure laser parameters for high-pressure thermometry measurements. In the second part, spatially resolved H₂ temperature was measured in a rocket chamber at pressures up to 70 bar. This is the first demonstration of fs CARS thermometry inside a high-pressure rocket combustor. These results highlight the potential of using H₂ CPP fs CARS thermometry to provide quantitative data in high-pressure experiments for the study of combustion dynamics and model validation efforts at application relevant operating conditions.</p><p dir="ltr">The third chapter presents the development of a TCPS system for the study of the NO (<i>A</i>²Σ⁺-<i>X</i>²Π) state-to-state collision dynamics with He, Ar, and N₂. Two sets of TCPS spectra for 1% NO, diluted in different buffer gases at 295 K and 1 atm, were obtained with the pump beam tuned to the R₁₁(11.5) and ^OP₁₂(1.5) transitions. The probe was scanned while the pump beam was tuned to the line center. Collision induced transitions were observed in the spectra as the probe scanned over transitions that were not coupled with the pump frequency. The strength and structure of the collision induced transitions in the TCPS spectra were compared between the three colliding partners. Theoretical TCPS spectra, calculated by solving the density matrix formulation of the time-dependent Schrödinger wave equation, were compared with the experimental spectra. A collision model based on the modified exponential-gap law was used to model the rotational level-to-rotational level collision dynamics. An unique aspect of this work is that the collisional transfer from an initial to a final Zeeman state was modeled based on the difference in the cosine of the rotational quantum number <i>J</i> projection angle with the z-axis for the two Zeeman states. Rotational energy transfer rates and Zeeman state collisional dynamics were varied to obtain good agreement between theory and experiment for the two different TCPS pump transitions and for the three different buffer gases. One key finding, in agreement with quasi-classical trajectory calculations, is that the spin-rotation changing transition rate in the <i>A</i>²Σ⁺ level of NO is almost zero for rotational quantum numbers ≥ 8. It was necessary to set this rate to near zero to obtain agreement with the TCPS spectra. </p><p dir="ltr">The fourth chapter presents the development and application of a broadband ULAS technique operating in the mid-infrared for simultaneous measurements of temperature, methane (CH₄), and propane (C₃H₈) mole fractions. Single-shot measurements targeting the C-H stretch fundamental vibration bands of CH₄ and C₃H₈ near 3.3 μm were acquired in both a heated gas cell up to ~650 K and laminar diffusion flames at 5 kHz. The average temperature error is 0.6%. The average species mole fraction error are 5.4% for CH₄, and 9.9% for C₃H₈. This demonstrates that ULAS is capable of providing high-fidelity hydrocarbon-based thermometry and simultaneous measurements of both large and small hydrocarbons in combustion gases. </p>

Rocket propulsion using the hybrid-propellant scheme is a technology that offers much promise in applications where high-performance liquid rocket engines are deemed too complex and solid rocket motors are considered to lack performance or safety. However, despite extensive research, there is still a lack of knowledge in the theoretical aspects of hybrid rocketry, especially in the area of fuel-oxidizer mixing and fuel regression rate. This lack of a good theoretical model makes the implementation of good, practical solutions and mature, well-functioning designs more diffcult. This disadvantages the hybrid rocket engine when compared to liquid rocket engines or solid rocket motors.In this study, a hybrid rocket engine burning polymethyl methacrylate (PMMA) with compressed air has been designed to the point of a preliminary design defnition. PMMA is a transparent material, and this has been utilized to create a transparent-chamber rocket engine where engine processes can be studied with various optical methods withoutinterrupting or disturbing the operation of the engine. The function of hybrid rocket engines, the technological solutions involved in designing working hybrid rocket engines and the constituent parts of hybrid rocket engines have been studied. The nature of the trade-offs between performance and simplicity that occur when designing a rocket engine are also studied, with a focus on maximizing simplicity, safety and minimizing expenses, while still designing an engine that fulfills basic requirements. The results include a design defnition with a preliminary user’s guide, a feasibility study, and a summary of the results of the hybrid rocket performance model that was used to determine appropriate design parameters.

<p dir="ltr">Laser absorption spectroscopy (LAS) is a widely used technique to acquire path-integrated measurements of gas properties such as temperature and mole fraction. Although extremely useful, the application of LAS to study heterogeneous combustion environments can be challenging. For example, beam steering can be one such challenge that arises during measurements in heterogeneous combustion environments such as metallized propellant flames or measurements at high-pressure conditions. The ability to only obtain path integrated measurements has been a major challenge of conventional LAS techniques, especially in characterizing combustion environments with a non-uniform thermo-chemical distribution along the line of sight (LOS). Additionally, simultaneous measurements of multiple species using LAS with narrow-bandwidth lasers often necessitates employing multiple light sources. Aerospace applications, such as characterizing hypersonic flows may require ultrashort time resolution to study fast-evolving chemistry. Similarly, atmospheric entry most often requires measurements of atoms and molecules that absorb at wavelengths ranging from ultraviolet to mid-infrared. The availability of appropriate light sources for such measurements has been limited. In the past, several researchers have come up with diagnostic techniques to overcome the above-mentioned challenges to a certain extent. Most often, these solutions have been need-based while compromising on other diagnostic capabilities. Therefore, LAS diagnostics capable of acquiring broadband measurements with ultrafast time resolution and the ability to acquire measurements at wavelengths in ultraviolet through mid-infrared is required to study advanced combustion systems and for the development of advanced aerospace systems for future space missions. Ultrafast laser absorption spectroscopy is one such technique that provides broadband measurements, enabling simultaneous multi-species and high-pressure measurements. The light source utilized for ULAS provides the ultrafast time resolution necessary for resolving fast-occurring chemistry and more importantly the ability to acquire measurements at a wide range of wavelengths ranging from ultraviolet to far-infrared. The development and application of ULAS for characterizing propellant flames and hypersonic flows under non-equilibrium conditions by overcoming the above-mentioned challenges is presented here. </p><p>This work describes the development of a single-shot ultrafast laser absorption spectroscopy (ULAS) diagnostic for simultaneous measurements of temperature and concentrations of CO, NO, and H₂O in flames and aluminized fireballs of HMX (C₄H₈N₈O₈). Ultrashort (55 fs) pulses from a Ti:Sapphire oscillator emitting near 800 nm were amplified and converted into the mid-infrared through optical parametric amplification (OPA) at a repetition rate of 5 kHz. Ultimately, pulses with a spectral bandwidth of ≈600 cm^-1 centered near 4.9 µm were utilized in combination with a mid-infrared spectrograph to measure absorbance spectra of CO, NO, and H₂O across a 30 nm bandwidth with a spectral resolution of 0.3 nm. The gas temperature and species concentrations were determined by least-squares fitting simulated absorbance spectra to measured absorbance spectra. Measurements of temperature, CO, NO, and H₂O were acquired in an HMX flame burning in air at atmospheric pressure and the measurements agree well with previously published results. Measurements were also acquired in fireballs of HMX with and without 16.7 wt% H-5 micro-aluminum. Time histories of temperature and column densities are reported with a 1-σ precision of 0.4% for temperature and 0.3% (CO), 0.6% (NO), and 0.5% (H₂O), and 95% confidence intervals (C.I.) of 2.5% for temperature and 2.5% (CO), 11% (NO), and 7% (H₂O), thereby demonstrating the ability of ULAS to provide high-fidelity, multi-parameter measurements in harsh combustion environments. The results indicate that the addition of the micron-aluminum increases the fireball peak temperature by ≈100 K and leads to larger concentrations of CO. The addition of aluminum also increases the duration fireballs remain at elevated temperatures above 2000 K.</p><p dir="ltr">Next, the application of ULAS for dual-zone temperature and multi-species (CO, NO, H₂O, CO₂, HCl, and HF) measurements in solid-propellant flames is presented. ULAS measurements were acquired at three different central wavelengths (5.121 µm, 4.18 µm, and 3.044 µm) for simultaneous measurements of temperature and: 1) CO, NO, and H₂O, 2) CO₂ and HCl, and 3) HF and H₂O. Absorption measurements with a spectral resolution of 0.35 nm and bandwidth of 7 cm^-1, 18 cm^-1, and 35 cm^-1, respectively were acquired. In some cases, a dual-zone absorption spectroscopy model was implemented to accurately determine the gas temperature in the hot flame core and cold flame boundary layer via broadband absorption measurements of CO₂, thereby overcoming the impact of line-of-sight non-uniformities. Results illustrate that the hot-zone temperature of CO₂ agrees well with the equilibrium flame temperature and single-zone thermometry of CO, the latter of which is insensitive to the cold boundary layer due to the corresponding oxidation of CO to CO₂.</p><p dir="ltr">The initial development and implementation of an ultraviolet and broadband ultrafast-laser-absorption-imaging (UV-ULAI) diagnostic for one dimensional (1D) imaging of temperature and CN via its <i>B</i>²Σ⁺←<i>X</i>²Σ⁺absorption bands near 385 nm. The diagnostic was demonstrated by acquiring single-shot measurements of 1D temperature and CN profiles in HMX flames at a repetition rate of 25 Hz. Ultrashort pulses (55 fs) at 800 nm were generated using a Ti:Sapphire oscillator and then amplification and wavelength conversion to the ultraviolet was carried out utilizing an optical parametric amplifier and frequency doubling crystals. The broadband pulses were spectrally resolved using a 1200 l/mm grating and imaged on an EMCCD camera to obtain CN absorbance spectra with a resolution of ≈0.065 nm and a bandwidth of ≈4 nm (i.e. 260 cm^-1). Simulated absorbance spectra of CN were fit to the measured absorbance spectra using non-linear curve fitting to determine the gas properties. The spatial evolution of gas temperature and CN concentration near the burning surface of an HMX flame was measured with a spatial resolution of ≈10 µm. 1D profiles of temperature and CN concentration were obtained with a 1-σ spatial precision of 49.3 K and 4 ppm. This work demonstrates the ability of UV-ULAI to acquire high-precision, spatially resolved absorption measurements with unprecedented temporal and spatial resolution. Further, this work lays the foundation for ultraviolet imaging of numerous atomic and molecular species with ultrafast time resolution.</p><p dir="ltr">Ultraviolet ULAS was applied to characterize the temporal evolution of non-Boltzmann CN (<i>X</i>²Σ⁺) formed behind strong shock waves in N₂-CH₄ mixtures at conditions relevant to entry into Titan's atmosphere. An ultrafast (femtosecond) light source was utilized to produce 55 fs pulses near 385 nm at a repetition rate of 5 kHz and a spectrometer with a 2400 lines/mm grating was utilized to spectrally resolve the pulses after passing through the Purdue High-Pressure Shock Tube. This enabled broadband single-shot absorption measurements of CN to be acquired with a spectral resolution and bandwidth of ≈0.02 nm and ≈6 nm (≈402 cm^-1 at these wavelengths), respectively. A line-by-line absorption spectroscopy model for the <i>B</i>²Σ⁺←<i>X</i>²Σ⁺ system of CN was developed and utilized to determine six internal temperatures (two vibrational temperatures, four rotational) of CN from the (0,0), (1,1), (2,2) and (3,3) absorption bands. Measurements were acquired behind reflected shock waves in 5.65% CH₄ and 94.35% N₂ with an initial pressure of 1.56 mbar and incident shock speed of ≈2.1 km/s. For this test condition, the chemically and vibrationally frozen temperature of the mixture behind the reflected shock was 5000 K and the pressure was 0.6 atm. The high repeatability of the shock-tube experiments (0.3% variation in shock speed across tests) enabled multi-shock time histories of CN mole fraction and six internal temperatures to be acquired with a single-shot time resolution of less than 1 ns. The measurements revealed that CN <i>X</i>²Σ⁺ is non-Boltzmann rotationally and vibrationally for greater than 200 µs, thereby strongly suggesting that chemical reactions are responsible for the non-Boltzmann population distributions. </p><p><br></p>

No description available.