Theo Guillaume’s research while affiliated with University of Birmingham and other places

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Publications (19)


HILTRAC apparatus schematic and inset photos. The apparatus schematic highlights the movable Chamber 1, the path of the UV photolysis laser (light blue), the reservoir with gas inlets (purple arrows), the USF produced from the nozzle, and the intersection of the flow with the DFCS (red) and LIF (green) optical axes. The top inset photos show the reservoir with the Laval nozzle (left) and the Pitot tube mounted on the YZ translation stages (right). The bottom inset photo shows an interior picture of the chamber, with the X translation stage for the reservoir visible on the internal breadboard, the two optical axes for LIF and DFCS overlapping with the UV photolysis laser, and the cage-mounted LIF collection optics. A red diode laser shows the approximate path of the infrared frequency comb laser beam as it reflects off the gold mirrors for the Herriott multipass configuration. Further detail is in the text.
Contour map (bottom left) of the USF in an Ar buffer gas for Nozzle 9 from 1 to 50 cm in X and −1.8 to 1.8 cm in Y in 0.2 cm intervals in both cases, interpolated to help with visualization. In addition, shown is a 1D profile in the X plane at Y = 0 cm (top) and a 1D profile in the Y plane at X = 15 cm (bottom right).
Experimental (red) LIF spectrum of CH B ²Σ⁻–X ²Π (1, 0), with fluorescence detected around 400 nm on the (1, 1) transition. A PGOPHER simulation is overlaid (black) and used to fit the observed rotational temperature to a temperature of 40(2) K. Note that the Q2(1) transition is primarily used in the reported kinetics studies.
Infrared spectrum of OCS from 2897 to 2932 cm⁻¹ (black, panel A) compared against a PGOPHER simulation (red, panel A) using a temperature of 49.5 K and a Gaussian broadening FWHM of 0.002 23 cm⁻¹. A few asterisks mark out some anomalous data points, which are not considered real signals as each only appears at a single repetition rate and not any other repetition rate data point directly adjacent. The inset in panel B shows a narrow wavenumber region near 2900 cm⁻¹, highlighting absorption features due to OC³⁴S and potentially OCS-Ar, discussed further in the text. While the experimental data in black in all three panels are the final interleaved spectrum, the spectrum collected at a single repetition rate (249.999 800 MHz) is shown in panel C, with the blue symbols showing the discrete measured absorbances at each comb tooth. In addition, shown in panel C are the residuals between the experiment and the PGOPHER simulation. Note that all red traces (PGOPHER simulation) are inverted for clarity.
Representative normalized transient CH integrated fluorescence signal as a function of laser delay time taken at 32(3) K and a total density of 4(1) × 10¹⁶ molecule cm⁻³, together with single exponential decay fits for [OCS] = 0.00 (black), 7.73 × 10¹² (blue), 4.50 × 10¹³ (red), and 1.54 × 10¹⁴ (green) molecule cm⁻³, respectively.

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Design and implementation of a new apparatus for astrochemistry: Kinetic measurements of the CH + OCS reaction and frequency comb spectroscopy in a cold uniform supersonic flow
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September 2024

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48 Reads

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2 Citations

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Théo Guillaume

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Julia H. Lehman

We present the development of a new astrochemical research tool, HILTRAC, the Highly Instrumented Low Temperature ReAction Chamber. The instrument is based on a pulsed form of the CRESU (Cinétique de Réaction en Écoulement Supersonique Uniforme, meaning reaction kinetics in a uniform supersonic flow) apparatus, with the aim of collecting kinetics and spectroscopic information on gas phase chemical reactions important in interstellar space or planetary atmospheres. We discuss the apparatus design and its flexibility, the implementation of pulsed laser photolysis followed by laser induced fluorescence, and the first implementation of direct infrared frequency comb spectroscopy (DFCS) coupled to the uniform supersonic flow. Achievable flow temperatures range from 32(3) to 111(9) K, characterizing a total of five Laval nozzles for use with N2 and Ar buffer gases by impact pressure measurements. These results were further validated using LIF and direct frequency comb spectroscopy measurements of the CH radical and OCS, respectively. Spectroscopic constants and linelists for OCS are reported for the 10⁰1 band near 2890–2940 cm⁻¹ for both OC³²S and OC³⁴S, measured using DFCS. Additional peaks in the spectrum are tentatively assigned to the OCS-Ar complex. The first reaction rate coefficients for the CH + OCS reaction measured between 32(3) and 58(5) K are reported. The reaction rate coefficient at 32(3) K was measured to be 3.9(4) × 10⁻¹⁰ cm³ molecule⁻¹ s⁻¹ and the reaction was found to exhibit no observable temperature dependence over this low temperature range.

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Developing a predictive model for low-temperature Laval nozzles with applications in chemical kinetics

July 2024

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68 Reads

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2 Citations

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Laval nozzles are used in the CRESU (“Cinétique de Réaction en Écoulement Supersonique Uniforme”) method to generate a collimated low temperature (5–200 K), low pressure (30–500 Pa), high Mach number (1 < M < 20) supersonic jet. Laval nozzles have been designed using the Method of Characteristics (MOC) since the development of CRESU, which is an analytical method that assumes inviscid, isentropic flow, and is routinely used to design nozzle profiles for a particular gas and temperature with a uniform shock free exit. This study aims to provide a robust computational framework to overcome the limitations of the MOC while also providing recommendations on the numerical model setup required to model a low-temperature supersonic jet. It also discusses the blockage effects when using the Pitot tube method for flow characterization, the influence of inlet turbulence and reservoir size. Numerical results are validated using two different experimental apparatuses from research groups at the University of Leeds and the University of Birmingham. Finally, a MATLAB framework was developed and has been provided as an open source toolbox to allow any user to perform computational fluid dynamics on any Laval nozzle, with the ability to change nozzle geometry, operating conditions and bath gas. The toolbox has been rigorously tested against many benchmark cases, which shows that steady-state Reynolds-averaged Navier–Stokes with the k-omega-shear stress transport turbulence model can be used to accurately predict global quantities, such as average temperature in the stable region of the supersonic jet.


Figure 2. Contour map (bottom left) of the USF in an Ar buffer gas for Nozzle 9 from 1 -50 cm in X and -1.8 -1.8 cm in Y in 0.2 cm intervals in both cases. Also shown is a 1D profile in the X plane at Y = 0 cm (top) and a 1D profile in the Y plane at X = 15 cm (bottom right).
Figure 3. Experimental (red) LIF spectrum of CH B 2 Σ --X 2 Π (1, 0), with fluorescence detected around 400 nm on the (1, 1) transition. A PGOPHER simulation is overlaid (black) and used to fit the observed rotational temperature to a temperature of 40(2) K. Note that the Q2(1) transition is primarily used in the reported kinetics studies.
Figure 4. Infrared spectrum of OCS from 2897 -2932 cm -1 (black, panel A) compared against a PGOPHER simulation (red, panel A) using a temperature of 49.5 K and a Gaussian broadening FWHM of 0.00223 cm -1 . The inset in panel B shows a narrow wavenumber region near 2900 cm -1 , highlighting absorption features due to OC 34 S and potentially OCS-Ar, discussed further in the text. While the experimental data in black in all three panels is the final interleaved spectrum, the spectrum collected at a single repetition rate (249.999800 MHz) is shown in panel C, with the blue symbols showing the discrete measured absorbances at each comb tooth. Also shown in panel C are the residuals between the experiment and the PGOPHER simulation. Note that all red traces (PGOPHER simulation) are inverted for clarity.
Figure 6. Loss rate of CH as a function of OCS density at 32(3) K, a total density of 4(1)  10 16 molecule cm -3 and [CHBr3] = 4.5  10 12 molecule cm -3 with linear fits to determine k(32(3) K) and 95% confidence bands. A: Study to determine the [OCS] concentration at which curvature is observed. Data where [OCS] > 8  10 13 molecule cm -3 were excluded from the fit as indicated by the purple line. k(32(3) K) = 4.0(1)  10 -10 cm 3 molecule -1 s -1 . B: Data for 8.7  10 12 molecule cm -3 (blue), [CHBr3] = 4.0  10 12 molecule cm -3 (black), and 1.9  10 12 molecule cm -3 (green), using the Q2(1) transition at 363.432 nm. The second [CHBr3] used to examine the CH propensity using the Q1(1) transition at 363.668 nm (red). k(32(3) K) = 3.7(1)  10 -10 , 4.0(2)  10 -10 , 3.2(1)  10 -10 , and 3.7(1)  10 -10 cm 3 molecule -1 s -1 for the blue, black, green, and red data, respectively.
Design and Implementation of a New Apparatus for Astrochemistry: Kinetic Measurements of the CH + OCS Reaction and Frequency Comb Spectroscopy in a Cold Uniform Supersonic Flow

May 2024

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120 Reads

We present the development of a new astrochemical research tool HILTRAC, the Highly Instrumented Low Temperature ReAction Chamber. The instrument is based on a pulsed form of the CRESU (Cin\'etique de R\'eaction en \'Ecoulement Supersonique Uniforme, meaning reaction kinetics in a uniform supersonic flow) apparatus, with the aim of collecting kinetics and spectroscopic information on gas phase chemical reactions important in interstellar space or planetary atmospheres. We discuss the apparatus design and its flexibility, the implementation of pulsed laser photolysis followed by laser induced fluorescence (PLP-LIF), and the first implementation of direct infrared frequency comb spectroscopy (DFCS) coupled to the uniform supersonic flow. Achievable flow temperatures range from 32(3) - 111(9) K, characterising a total of five Laval nozzles for use with N2 and Ar buffer gases by pressure impact measurements. These results were further validated using LIF and DFCS measurements of the CH radical and OCS, respectively. Spectroscopic constants and linelists for OCS are reported for the 1001 band near 28902940cm12890 - 2940 cm^{-1} for both OC32SOC^{32}S and OC34SOC^{34}S, measured using DFCS. Additional peaks in the spectrum are tentatively assigned to the OCS-Ar complex. The first reaction rate coefficients for the CH + OCS reaction measured between 32(3) K and 58(5) K are reported. The reaction rate coefficient at 32(3) K was measured to be 3.9(4)×1010cm3molecule1s13.9(4) \times 10^{10} cm^3 molecule^{-1} s^{-1} and the reaction was found to exhibit no observable temperature dependence over this low temperature range.


Product-specific reaction kinetics in continuous uniform supersonic flows probed by chirped-pulse microwave spectroscopy

May 2024

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22 Reads

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9 Citations

Experimental studies of the products of elementary gas-phase chemical reactions occurring at low temperatures (<50 K) are very scarce, but of importance for fundamental studies of reaction dynamics, comparisons with high-level quantum dynamical calculations, and, in particular, for providing data for the modeling of cold astrophysical environments, such as dense interstellar clouds, the atmospheres of the outer planets, and cometary comae. This study describes the construction and testing of a new apparatus designed to measure product branching fractions of elementary bimolecular gas-phase reactions at low temperatures. It combines chirped-pulse Fourier transform millimeter wave spectroscopy with continuous uniform supersonic flows and high repetition rate laser photolysis. After a comprehensive description of the apparatus, the experimental procedures and data processing protocols used for signal recovery, the capabilities of the instrument are explored by the study of the photodissociation of acrylonitrile and the detection of two of its photoproducts, HC3N and HCN. A description is then given of a study of the reactions of the CN radical with C2H2 at 30 K, detecting the HC3N product, and with C2H6 at 10 K, detecting the HCN product. A calibration of these two products is finally attempted using the photodissociation of acrylonitrile as a reference process. The limitations and possible improvements in the instrument are discussed in conclusion.


Schematic view of the experiment with 2D density map and T2 decay times
a, Schematic of the experiment showing a uniform helium flow from a Laval nozzle. The cold core of the flow is illuminated by a pulsed 193 nm laser, generating HCN and HNC molecules in situ by photolysis of vinyl cyanide, which are then detected downstream from the nozzle exit by the CPFTmmW spectrometer. b, An example 2D density map taken from Pitot measurements under 16 K conditions in a helium flow, showing the higher-density isentropic core giving way to the boundary regions, where the density drops rapidly and the temperature increases. Shown are the interpolated data between the original 0.25 × 1 cm point spacing of the experimentally measured grid. The region that the spectrometer probes is indicated. The map is completed by a computational fluid dynamics simulation for the flow within the nozzle using Ansys Fluent, capped at a maximum density of 1 × 10¹⁷ cm⁻³ (otherwise the much higher density in the throat of the nozzle would compress the scale of the whole map). c, Measurements of the T2 decay time as a function of time after the laser shot. The time axis is scaled to the distance from the nozzle exit in b, as under uniform conditions the molecules moving through the detection zone will be formed at a given position that can be correlated to time. The shaded areas around the T2 decay times represent the 95% confidence intervals for fitting the Voigt profile at each point along the uniform flow. Each T2 decay time results from fitting of an FID which is an average of 10⁵ laser shots. The difference in T2 decay times for the two isomers can be clearly seen.
Examples of fits to FIDs for HCN and HNC in helium at 16 K
a, Time domain experimental data (black) and the fit (red) obtained using Supplementary Information, equation (1) for HCN. Inset: zoomed version for 5 ns. arb., arbitrary. b, FFTs of the data and the fit for HCN shown in a. c, Time-domain experimental data (black) and the fit (blue) obtained for HNC using a time-domain Voigt single-frequency function as in Hays et al.²⁷. d, FFTs of the data and the fit for HNC shown in c. e, Demodulated decay profiles of fitted data for HCN (red) and HNC (blue). Panels b and d show the FFT of the time domain fits which represent the FFTs of the original data well, highlighting the robustness of fitting the time-domain data. The demodulated decay profiles for each molecule show the fitted exponential decays of the frequency components for the molecules. The decay times (T2), recorded under similar conditions, are clearly different, with the decay being faster for HNC than for HCN, reflecting the different helium pressure-broadening cross-sections. All data displayed result from the averaging of FIDs recorded from 10⁵ laser shots.
Theoretical and experimental pressure-broadening cross sections for HCN and HNC with helium
Results from this study are compared to those from other experiments, including empirical fits to HC¹⁵N data. Error bars for the current experiments correspond to 95% confidence intervals from the averaging of the measured T2 decay times combined with contributions from estimated possible systematic errors in the flow density and temperature of 10% (see Supplementary Information, section 1A for further details). Error bars from other work correspond to 2σ when available. Previous data for HCN are from refs. ³¹,32. The new experimental data and scattering calculations display very good agreement over the temperature range 10–70 K. Both species show a rising trend in pressure-broadening cross sections with decreasing temperature, with the cross sections for HNC being higher than for HCN over this temperature range. This reflects a stronger collisional excitation of HNC than HCN by helium (and by implication H2), especially at the low temperatures found in dense interstellar clouds. This strongly affects the observed HNC/HCN abundance ratio and helps explain the anomalously high values that have previously been reported.
Collisional excitation of HNC by He found to be stronger than for structural isomer HCN in experiments at the low temperatures of interstellar space

July 2022

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250 Reads

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13 Citations

Nature Chemistry

HCN and its unstable isomer HNC are widely observed throughout the interstellar medium, with the HNC/HCN abundance ratio correlating strongly with temperature. In very cold environments HNC can even appear more abundant than HCN. Here we use a chirped pulse Fourier transform spectrometer to measure the pressure broadening of HCN and HNC, simultaneously formed in situ by laser photolysis and cooled to low temperatures in uniform supersonic flows of helium. Despite the apparent similarity of these systems, we find the HNC–He cross section to be more than twice as big as the HCN–He cross section at 10 K, confirming earlier quantum calculations. Our experimental results are supported by high-level scattering calculations and are also expected to apply with para-H2, demonstrating that HCN and HNC have different collisional excitation properties that strongly influence the derived interstellar abundances. HCN and its isomer HNC are both observed in the interstellar medium and inelastic collisions with helium and other species strongly influence their derived abundances. Now it has been shown experimentally and theoretically that HNC is much more strongly excited than HCN in collisions with helium at the low temperatures of interstellar space.




Construction of an E-band chirped pulse spectrometer and application to the measurement of low temperature collisional processes of astrochemical interest

October 2021

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13 Reads

This thesis presents research work on the construction and development of a new instrument and its utilization in the framework of the CPUF technique (Chirped Pulse in Uniform Flow) to study low-temperature collisional processes of astrochemical interest. The thesis details the characteristics of the CRESUCHIRP apparatus and the technical development related to its utilization as a CPUF instrument. The new CRESU (Cinétique de Réaction en Écoulement supersonique Uniforme) apparatus and the supporting instrumentation are described. The characterization of an E-band (60-90 GHz) CP-FTmmW spectrometer (Chirped Pulse-Fourier Transform millimeter Wave) is presented with its coupling to the rest of the instrument. The capability of the spectrometer as a spectroscopic tool is presented with the measurement of pressure broadening coefficients at room temperature for the system OCS + He. Experiments using the CPUF technique are presented with the measurement of the difference in collisional interaction of isomers at low temperatures: HCN and HNC with He. Studies of the potential of the instrument for application to kinetics measurement at low temperature are presented for the reactions CN + ethane at 10 K and CN + acetylene at 30 K. Tentative calibrations of these two reactions are presented. The strengths and weaknesses of the new instrument are discussed, as well as potential improvements to the technique.




Citations (7)


... 33 Infrared absorption spectroscopy has also been coupled with uniform Laval flow experiments using single-frequency lasers 34,35 and broadband light sources. 36,37 The extended interaction path length between the light and sample achieved by cavity-enhanced techniques is desired to increase sensitivity for detecting trace species during reactions. ...

Reference:

A new apparatus for gas-phase low temperature kinetics study: Kinetics measurement and product detection of the CH + propene reaction at 23 K
Design and implementation of a new apparatus for astrochemistry: Kinetic measurements of the CH + OCS reaction and frequency comb spectroscopy in a cold uniform supersonic flow

... Complementary computational fluid dynamics simulations are currently underway to fully characterize and optimize the flow conditions and nozzle design. 65 Eventually, the uniformity of the flow breaks down, invalidating the Rayleigh-Pitot equations. For kinetics purposes, it is necessary to know when the uniform temperature and density conditions are no longer maintained. ...

Developing a predictive model for low-temperature Laval nozzles with applications in chemical kinetics

... We therefore give here a comprehensive description of the production and detecton schemes. BrC 3 N was chosen as a photolytic precursor by analogy with CN radicals which can be produced by laser photolysis of BrCN as in Guillaume et al. (2024). The synthesis of the precursor was adapted from the description available in the literature. ...

Product-specific reaction kinetics in continuous uniform supersonic flows probed by chirped-pulse microwave spectroscopy

... Techniques developed to meet this challenge include ion cyclotron resonance, 11 flowing afterglow, 12 heavy ion storage rings, 13 and CRESU. 14 This last technique is able to study ion-neutral and neutral-neutral reactions at temperatures as low as 10 K, 15,16 but requires a very large pumping capacity. 14 Theoretical treatments also exist for calculating reaction rate coefficients, however, highly-accurate ab initio potential energy surfaces are often needed, as the presence of small barriers can significantly affect calculated rate coefficients. ...

Collisional excitation of HNC by He found to be stronger than for structural isomer HCN in experiments at the low temperatures of interstellar space

Nature Chemistry

... A new experimental apparatus, dedicated to the measurement of reaction product branching ratios using the CPUF technique, has been developed. This included the construction of a new CRESU apparatus and two new CP-FTmmW spectrometers operating in the Ka-band (26)(27)(28)(29)(30)(31)(32)(33)(34)(35)(36)(37)(38)(39)(40) and E-band (60-90 GHz). The design and performance of the two spectrometers are discussed in detail in Hays et al. 24 and Hearne et al. 28 The design of the new CRESU chamber for CPUF experiments (the CRESUCHIRP chamber) is outlined in Sec. ...

A novel Ka-band chirped-pulse spectrometer used in the determination of pressure broadening coefficients of astrochemical molecules
  • Citing Article
  • August 2020

... 59 More recently, a chirped-pulse Fourier transform microwave spectrometer has been coupled to the USF. 38,43,60,61 Microwave spectroscopy employed in this manner allows for a wide frequency range to be detected, collecting detailed spectroscopic and structural information about the molecules present in the USF. More than one species can potentially be monitored simultaneously, such as by observing reaction products. ...

Design and performance of an E-band chirped pulse spectrometer for kinetics applications: OCS – He pressure broadening
  • Citing Article
  • July 2020

Journal of Quantitative Spectroscopy and Radiative Transfer

... Pulsed laser photolysis followed by laser induced fluorescence (PLP-LIF) is one method that is ubiquitous in the field of gas-phase chemical kinetics. [48][49][50][51][52][53][54] The PLP-LIF method allows one to initiate a reaction, then probe a specific rovibronic transition of the molecule of interest (typically a radical reactant) and collect its fluorescence as a function of reaction time to obtain the relative concentration of the species of interest. 27 While LIF is highly selective for the molecule of interest, quantitative product branching fractions, although possible, are difficult to obtain from this method. ...

Low Temperature Kinetics of the Reaction Between Methanol and the CN Radical
  • Citing Article
  • October 2019

The Journal of Physical Chemistry A