Robert Wendell Pitz
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Robert Wendell Pitz has a total of 181 co-authors. Here are the top co-authors by number of shared publications:
Shengteng Hu
10 shared publicationsJoseph A. Wehrmeyer
Aerospace Testing Alliance, Building 1099, Avenue C, Arnold Air Force Base, TN 37389, USA
9 shared publicationsPeiyong Wang
6 shared publicationsJ.A. Wehrmeyer
5 shared publicationsMarshall Lapp
General Electric Corporate Research and Development, Schenectady, NY 12345, U.S.A.
5 shared publicationsMichael C. Drake
5 shared publications
Latest Publications
- Open Access
- 9 October 2026
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 42
The effects of hydrogen addition on the structural characteristics and combustion stability of single premixed tubular methane flames
- 9 October 2026
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 42
Open AccessThe effects of hydrogen addition on the structural characteristics and combustion stability of single premixed tubular methane flames
- Open Access
- 8 September 2026
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 37 (36) , 365201
Hybrid 2D method for molecular tagging velocimetry with application to supersonic flow over a bluff-body with a centerline fuel-jet
A hybrid method for 2D molecular tagging velocimetry is developed to overcome the limitations of template-based methods in high-speed flows. The method integrates a Hough line transform for grid detection at arbitrary grid orientations with a multi-scale optical-flow method for sub-pixel tracking of intersections. The method was validated using synthetic datasets, achieving < 0.1 pixel root-mean-square error for translational and shear-dominated flows for signal-to-noise ratio ⩾ 4. The method is applied to analyze experimental hydroxyl tagging velocimetry measurements in a Mach 1.5 supersonic flow over an axisymmetric bluff-body with a centerline sonic N 2 fuel-jet. Time-resolved imaging of a photodissociated 11 × 11 OH grid reveals the complex velocity field, capturing a high-speed supersonic fuel-jet, expansion waves, shear layers, and the recirculation zone behind the bluff-body. By eliminating template dependency, this method provides robust, automated, and accurate velocity fields for validating high-fidelity computational fluid dynamics simulations.
- 8 September 2026
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 37 (36) , 365201
Open AccessHybrid 2D method for molecular tagging velocimetry with application to supersonic flow over a bluff-body with a centerline fuel-jet
A hybrid method for 2D molecular tagging velocimetry is developed to overcome the limitations of template-based methods in high-speed flows. The method integrates a Hough line transform for grid detection at arbitrary grid orientations with a multi-scale optical-flow method for sub-pixel tracking of intersections. The method was validated using synthetic datasets, achieving < 0.1 pixel root-mean-square error for translational and shear-dominated flows for signal-to-noise ratio ⩾ 4. The method is applied to analyze experimental hydroxyl tagging velocimetry measurements in a Mach 1.5 supersonic flow over an axisymmetric bluff-body with a centerline sonic N 2 fuel-jet. Time-resolved imaging of a photodissociated 11 × 11 OH grid reveals the complex velocity field, capturing a high-speed supersonic fuel-jet, expansion waves, shear layers, and the recirculation zone behind the bluff-body. By eliminating template dependency, this method provides robust, automated, and accurate velocity fields for validating high-fidelity computational fluid dynamics simulations.
- Open Access
- 27 February 2025
- Published by Elsevier in Combustion and Flame
- Vol. 275
Numerical study of heat release rate indicators in 1D and 2D atmospheric and high pressure premixed ammonia-air and ammonia-hydrogen-air tubular flames
- 27 February 2025
- Published by Elsevier in Combustion and Flame
- Vol. 275
Open AccessNumerical study of heat release rate indicators in 1D and 2D atmospheric and high pressure premixed ammonia-air and ammonia-hydrogen-air tubular flames
- 1 September 2021
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 37 (5) , 748-758
Cylindrical Air-Gap Electrode Spark Discharge Characterization and Quenching
Spark discharges were parametrically examined for a cylindrical air-gap electrode configuration. The aim of this study was to elucidate spark discharge characteristics, arc penetration, and exhaust plume development to guide designers of relevant ignition devices. Spark gaps ranged from 0.5 to 2.3 mm, nominal pressures ranged from 150 to 2200 kPa, and two exciter types (bipolar and unipolar) were tested. Positive correlations were observed between the pressure–distance product and multiple dependent variables: breakdown voltage, energy discharged, and percentage of sparks quenched. Positive correlations were observed between the pressure–distance quotient and various other dependent variables: spark duration, channel resistance, and plume velocity. This study also discusses the effects of quenching on electrical measurements, how these effects are nontrivial, and the subtle irregularities in electrical results that are indicative of quenching.
- 1 September 2021
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 37 (5) , 748-758
Cylindrical Air-Gap Electrode Spark Discharge Characterization and Quenching
Spark discharges were parametrically examined for a cylindrical air-gap electrode configuration. The aim of this study was to elucidate spark discharge characteristics, arc penetration, and exhaust plume development to guide designers of relevant ignition devices. Spark gaps ranged from 0.5 to 2.3 mm, nominal pressures ranged from 150 to 2200 kPa, and two exciter types (bipolar and unipolar) were tested. Positive correlations were observed between the pressure–distance product and multiple dependent variables: breakdown voltage, energy discharged, and percentage of sparks quenched. Positive correlations were observed between the pressure–distance quotient and various other dependent variables: spark duration, channel resistance, and plume velocity. This study also discusses the effects of quenching on electrical measurements, how these effects are nontrivial, and the subtle irregularities in electrical results that are indicative of quenching.
- Open Access
Numerical Study of the Structure and NO Emission Characteristics of N2- and CO2-Diluted Tubular Diffusion Flames
The structure of methane/air tubular diffusion flames with fuel dilution by either CO2 or N2 is numerically investigated as a function of pressure. As pressure is increased, the reaction zone thickness reduces due to decrease in diffusivities with pressure. The flame with CO2-diluted fuel exhibits much lower nitrogen radicals (N, NH, HCN, NCO) and lower temperature than its N2-diluted counterpart. In addition to flame structure, NO emission characteristics are studied using analysis of reaction rates and quantitative reaction pathway diagrams (QRPDs). Four different routes, namely the thermal route, Fenimore prompt route, N2O route, and NNH route, are examined and it is observed that the Fenimore prompt route is the most dominant for both CO2- and N2-diuted cases at all values of pressure followed by NNH route, thermal route, and N2O route. This is due to low temperatures (below 1900 K) found in these highly diluted, stretched, and curved flames. Further, due to lower availability of N2 and nitrogen bearing radicals for the CO2-diluted cases, the reaction rates are orders of magnitude lower than their N2-diluted counterparts. This results in lower NO production for the CO2-diluted flame cases.Open AccessNumerical Study of the Structure and NO Emission Characteristics of N2- and CO2-Diluted Tubular Diffusion Flames
The structure of methane/air tubular diffusion flames with fuel dilution by either CO2 or N2 is numerically investigated as a function of pressure. As pressure is increased, the reaction zone thickness reduces due to decrease in diffusivities with pressure. The flame with CO2-diluted fuel exhibits much lower nitrogen radicals (N, NH, HCN, NCO) and lower temperature than its N2-diluted counterpart. In addition to flame structure, NO emission characteristics are studied using analysis of reaction rates and quantitative reaction pathway diagrams (QRPDs). Four different routes, namely the thermal route, Fenimore prompt route, N2O route, and NNH route, are examined and it is observed that the Fenimore prompt route is the most dominant for both CO2- and N2-diuted cases at all values of pressure followed by NNH route, thermal route, and N2O route. This is due to low temperatures (below 1900 K) found in these highly diluted, stretched, and curved flames. Further, due to lower availability of N2 and nitrogen bearing radicals for the CO2-diluted cases, the reaction rates are orders of magnitude lower than their N2-diluted counterparts. This results in lower NO production for the CO2-diluted flame cases. - 1 January 2019
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 37 (2) , 2029-2036
Evaluation of heat release indicators in lean premixed H2/Air cellular tubular flames
- 1 January 2019
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 37 (2) , 2029-2036
Evaluation of heat release indicators in lean premixed H2/Air cellular tubular flames
- 1 January 2019
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 37 (2) , 2021-2028
Measurement and simulation of partially-premixed cellular tubular flames
- 1 January 2019
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 37 (2) , 2021-2028
Measurement and simulation of partially-premixed cellular tubular flames
- 1 December 2017
- Published by Elsevier in Combustion and Flame
- Vol. 186, 311-324
Raman/LIPF data of temperature and species concentrations in swirling hydrogen jet diffusion flames: Conditional analysis and comparison to laminar flamelets
- 1 December 2017
- Published by Elsevier in Combustion and Flame
- Vol. 186, 311-324
Raman/LIPF data of temperature and species concentrations in swirling hydrogen jet diffusion flames: Conditional analysis and comparison to laminar flamelets
- 10 July 2017
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 28 (8) , 085201
Molecular tagging velocimetry in nitrogen with trace water vapor
We report a new molecular tagging velocimetry method for use in pure nitrogen gas with a small impurity of water vapor on the order of 0.1%. This two laser method can produce a 25 mm long tag line of NH (imidogen) radicals at a standoff of 1 m which is imaged by laser-induced fluorescence after a delay of a few microseconds. The signal-to-noise ratio of the tag image can exceed 50 at standard temperature and pressure, allowing excellent spatial resolution. This new method called imidogen tagging velocimetry is useful for measuring spatially resolved velocity in flow facilities which run pure nitrogen rather than air, contain or can be seeded with trace water vapor, and in which other seeded or intrusive velocimetry methods are impractical.
- 10 July 2017
- Published by IOP Publishing in Measurement Science and Technology
- Vol. 28 (8) , 085201
Molecular tagging velocimetry in nitrogen with trace water vapor
We report a new molecular tagging velocimetry method for use in pure nitrogen gas with a small impurity of water vapor on the order of 0.1%. This two laser method can produce a 25 mm long tag line of NH (imidogen) radicals at a standoff of 1 m which is imaged by laser-induced fluorescence after a delay of a few microseconds. The signal-to-noise ratio of the tag image can exceed 50 at standard temperature and pressure, allowing excellent spatial resolution. This new method called imidogen tagging velocimetry is useful for measuring spatially resolved velocity in flow facilities which run pure nitrogen rather than air, contain or can be seeded with trace water vapor, and in which other seeded or intrusive velocimetry methods are impractical.