Pedro José Argumedo Teuffer
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Pedro José Argumedo Teuffer has a total of 14 co-authors. Here are the top co-authors by number of shared publications:
- Mario Alejandro Vega-Navarrete
Universidad Politécnica Metropolitana de Hidalgo, Mexico
3 shared publications - Carlos Manuel Rodríguez Roman
Department of Aerospace Engineering, Universidad Politécnica Metropolitana de Hidalgo, Tolcayuca 43860, Mexico
2 shared publications Alma Delia Paz Gómez
Metropolitan Polytechnic University of Hidalgo, México
1 shared publication- Carlos Roberto Dominguez Mayorga
Universidad Politécnica de Pachuca, México
1 shared publication - Francisco Marroquin-Gutierrez
Coordinación de Maestría en Ingeniería Aeroespacial, Universidad Politécnica Metropolitana de Hidalgo, Ex Hacienda San Javier, Tolcayuca 1009, Tolcayuca 43860, Hidalgo, Mexico
1 shared publication - Jean Fulbert Ituna Yudonago
Department of Aeronautical Engineering, Universidad Politécnica Metropolitana de Hidalgo, Tolcayuca, Mexico, Mexico
1 shared publication
Latest Publications
- 13 August 2026
- Published by IGI Global Scientific Publishing
- p. 195-232
Educational Strategies to Unleash Creativity and Soft Skills
This chapter presents an analysis of the relationship between creativity and soft skills within the contemporary educational context, highlighting their fundamental role in the training of agents capable of addressing the challenges of a society characterized by constant transformation, digitalization and the complexity of professional environments. The cognitive process is conceived from a sociocultural perspective, soft skills from a socioemotional, subjective and transversal perspective and the psychological perspective of the social agent as a trigger for autonomy, self-efficacy, self-sufficiency, self-regulation and metacognition, all of which together directly influences the agent's ability to manage learning, make decisions and adapt to different personal and professional situations. Based on this conceptual framework, various constructivist educational strategies are discussed to promote and develop creativity and interpersonal skills based on their explicit and structural integration in the curricular design.
- 13 August 2026
- Published by IGI Global Scientific Publishing
- p. 195-232
Educational Strategies to Unleash Creativity and Soft Skills
This chapter presents an analysis of the relationship between creativity and soft skills within the contemporary educational context, highlighting their fundamental role in the training of agents capable of addressing the challenges of a society characterized by constant transformation, digitalization and the complexity of professional environments. The cognitive process is conceived from a sociocultural perspective, soft skills from a socioemotional, subjective and transversal perspective and the psychological perspective of the social agent as a trigger for autonomy, self-efficacy, self-sufficiency, self-regulation and metacognition, all of which together directly influences the agent's ability to manage learning, make decisions and adapt to different personal and professional situations. Based on this conceptual framework, various constructivist educational strategies are discussed to promote and develop creativity and interpersonal skills based on their explicit and structural integration in the curricular design.
- Open Access
Analytical Study of Velocity Field Development in the Constrictor of a 200 kW Arc Jet
The following research focuses on the study of the behavior of air plasma developed inside a 200 kW arc-jet constrictor. The scope of the analysis performed in the present document is focused specifically on the velocity fields and their characteristics inside the constrictor domain. Among them, the velocity magnitude, the distribution of the radial profiles at different stations along the length of the constrictor, and the axial velocity profile distribution. The analytical study considers mathematical models, which include air properties like specific heat, thermal conductivity, electric conductivity and enthalpy. The axial enthalpy distribution is shown at different radii of the constrictor in order to explain the presence of the velocity fields inside the control volume of interest. In the present work, it was found that the magnitude of the air plasma velocity fields increases due to the contact with the electric arc along the constrictor, reaching maximum velocity values of 5000 m/s at 10,000 K in the center of the constrictor and gradually decreasing when the constrictor radius approaches the wall. These findings provide insight into performance aspects of an arc jet constrictor using atmospheric air as a propellant. A key limitation of the present study stems from the initial assumptions and restrictions detailed in the Materials and Methods section. These constraints inherently alter several plasma flow parameters, namely the Lorentz force, the radial variation of the electric potential, etc.
Open AccessAnalytical Study of Velocity Field Development in the Constrictor of a 200 kW Arc Jet
The following research focuses on the study of the behavior of air plasma developed inside a 200 kW arc-jet constrictor. The scope of the analysis performed in the present document is focused specifically on the velocity fields and their characteristics inside the constrictor domain. Among them, the velocity magnitude, the distribution of the radial profiles at different stations along the length of the constrictor, and the axial velocity profile distribution. The analytical study considers mathematical models, which include air properties like specific heat, thermal conductivity, electric conductivity and enthalpy. The axial enthalpy distribution is shown at different radii of the constrictor in order to explain the presence of the velocity fields inside the control volume of interest. In the present work, it was found that the magnitude of the air plasma velocity fields increases due to the contact with the electric arc along the constrictor, reaching maximum velocity values of 5000 m/s at 10,000 K in the center of the constrictor and gradually decreasing when the constrictor radius approaches the wall. These findings provide insight into performance aspects of an arc jet constrictor using atmospheric air as a propellant. A key limitation of the present study stems from the initial assumptions and restrictions detailed in the Materials and Methods section. These constraints inherently alter several plasma flow parameters, namely the Lorentz force, the radial variation of the electric potential, etc.
- Open Access
- 2 January 2026
- Published by Editorial Académica Dragón Azteca in International Journal of Combinatorial Optimization Problems and Informatics
- Vol. 17 (1) , 132-155
Identification and control of a Tail-Sitter Unmanned Aerial Vehicle
Unmanned aerial vehicles (UAVs) are increasingly employed in domains such as military operations, search-and-rescue missions, and surveillance. Recent research efforts have sought to integrate the advantages of fixed-wing and rotor-wing aircraft. Tail-sitter UAVs represent a class of hybrid platforms that combine rotor-wing vertical take-off and landing with fixed-wing forward-flight capability. These vehicles operate in three flight modes: vertical, horizontal, and transition. Depending on the transition mechanism, tail-sitter UAVs can be classified as mono-thrust transitioning (MTT), collective-thrust transitioning (CTT), or differential-thrust transitioning (DTT). Despite their potential, tail-sitter UAVs present substantial challenges in aerodynamic design and flight control, particularly with respect to instability and sensitivity to external disturbances. To address these issues, this work proposes an approach grounded in artificial intelligence and adaptive control principles. In particular, neural networks with tunable parameters, including inputs, weights, and transfer functions, are employed to enhance system robustness across varying operating conditions. Smart citations: https://scite.ai/reports/10.61467/2007.1558.2026.v17i1.1230 Dimensions.Open Alex.
- 2 January 2026
- Published by Editorial Académica Dragón Azteca in International Journal of Combinatorial Optimization Problems and Informatics
- Vol. 17 (1) , 132-155
Open AccessIdentification and control of a Tail-Sitter Unmanned Aerial Vehicle
Unmanned aerial vehicles (UAVs) are increasingly employed in domains such as military operations, search-and-rescue missions, and surveillance. Recent research efforts have sought to integrate the advantages of fixed-wing and rotor-wing aircraft. Tail-sitter UAVs represent a class of hybrid platforms that combine rotor-wing vertical take-off and landing with fixed-wing forward-flight capability. These vehicles operate in three flight modes: vertical, horizontal, and transition. Depending on the transition mechanism, tail-sitter UAVs can be classified as mono-thrust transitioning (MTT), collective-thrust transitioning (CTT), or differential-thrust transitioning (DTT). Despite their potential, tail-sitter UAVs present substantial challenges in aerodynamic design and flight control, particularly with respect to instability and sensitivity to external disturbances. To address these issues, this work proposes an approach grounded in artificial intelligence and adaptive control principles. In particular, neural networks with tunable parameters, including inputs, weights, and transfer functions, are employed to enhance system robustness across varying operating conditions. Smart citations: https://scite.ai/reports/10.61467/2007.1558.2026.v17i1.1230 Dimensions.Open Alex.
- Open Access
Geometric Design of a Low-Power Arcjet Constrictor and Determination of Velocity of Air-Based Plasma by Means of Analytical and Numerical Methods
The following research focuses on the analytical and numerical study of an arcjet constrictor. In order to perform these analyses, a geometric design of the constrictor was proposed. The analytical study considers mathematical models proposed by Stine and Watson, related to the properties of air propellants, such as the specific enthalpy, electric conductivity, thermal conductivity, and specific heat. The numerical study considered the equations for mass, momentum, energy, and electricity that describe the interaction between the electric arc and the fluid flow. These equations were solved in ANSYS FLUENT software, in which the - turbulence and the magnetohydrodynamic (MHD) models were used. The external routines, including user-defined functions, user-defined scalars, and user-defined memory were implemented in C++ language for source terms and linked to ANSYS FLUENT. The velocity profiles were obtained analytically for the electric arc temperatures of 9000 K, 10,000 K, and 11,000 K with peak magnitudes of 2960 m/s, 3350 m/s, and 3100 m/s, respectively, at the outlet of the constrictor. It was observed from the numerical results that the velocity magnitude of the air-based plasma inside the constrictor increases as the temperature of the electric arc rises up to 10,000 K However, above 10,000 K, the velocity magnitude decreases because at this temperature level, the air particles become completely ionized, and the specific heat of the air-based plasma decreases. The numerical simulation produced velocity profile magnitudes at two different electric arc temperatures (9000 K and 10,000 K) with peak magnitudes of 2400 m/s and 2900 m/s, respectively, at the outlet of the constrictor. The numerical and analytical results were very close with an error of 16.327%.Open AccessGeometric Design of a Low-Power Arcjet Constrictor and Determination of Velocity of Air-Based Plasma by Means of Analytical and Numerical Methods
The following research focuses on the analytical and numerical study of an arcjet constrictor. In order to perform these analyses, a geometric design of the constrictor was proposed. The analytical study considers mathematical models proposed by Stine and Watson, related to the properties of air propellants, such as the specific enthalpy, electric conductivity, thermal conductivity, and specific heat. The numerical study considered the equations for mass, momentum, energy, and electricity that describe the interaction between the electric arc and the fluid flow. These equations were solved in ANSYS FLUENT software, in which the - turbulence and the magnetohydrodynamic (MHD) models were used. The external routines, including user-defined functions, user-defined scalars, and user-defined memory were implemented in C++ language for source terms and linked to ANSYS FLUENT. The velocity profiles were obtained analytically for the electric arc temperatures of 9000 K, 10,000 K, and 11,000 K with peak magnitudes of 2960 m/s, 3350 m/s, and 3100 m/s, respectively, at the outlet of the constrictor. It was observed from the numerical results that the velocity magnitude of the air-based plasma inside the constrictor increases as the temperature of the electric arc rises up to 10,000 K However, above 10,000 K, the velocity magnitude decreases because at this temperature level, the air particles become completely ionized, and the specific heat of the air-based plasma decreases. The numerical simulation produced velocity profile magnitudes at two different electric arc temperatures (9000 K and 10,000 K) with peak magnitudes of 2400 m/s and 2900 m/s, respectively, at the outlet of the constrictor. The numerical and analytical results were very close with an error of 16.327%.