PEDRO DAVID BRAVO MOSQUERA

Pós-doutorado

Formação complementar

Idiomas

Áreas de atuação

Participação em eventos

Participação em bancas

Orientou

Produções bibliográficas

• GONZALEZ-DEGREIFF, PABLO ; GOMEZ-RIVERA, WILLIAM ; BRAVO-MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNAN D. . Numerical and experimental analysis of the effect of wavy leading edge on stabilizer. PHYSICS OF FLUIDS , v. 37, p. 065128, 2025.

• ABU SALEM, KARIM ; PALAIA, GIUSEPPE ; BRAVO-MOSQUERA, PEDRO D. ; QUARTA, ALESSANDRO A. . A Review of Novel and Non-Conventional Propulsion Integrations for Next-Generation Aircraft. Designs , v. 8, p. 20, 2024.

• GARCIA-RIBEIRO, DANIEL ; BRAVO-MOSQUERA, PEDRO D ; AYALA-ZULUAGA, JIMMY A ; MARTINEZ-CASTAÑEDA, DIEGO F ; VALBUENA-AGUILERA, JEISSON S ; CERÓN-MUÑOZ, HERNÁN D ; VACA-RIOS, JOHN J . Drag reduction of a commercial bus with add-on aerodynamic devices. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART D-JOURNAL OF AUTOMOBILE ENGINEERING , v. 237, p. 1623-1636, 2023.

• FLORES-MEZARINA, J.A. ; BRAVO-MOSQUERA, P.D. ; GARCIA-RIBEIRO, D. ; CERÓN-MUÑOZ, H.D. . Application of wavy leading edge to enhance winglet aerodynamic performance. AERONAUTICAL JOURNAL , v. 127, p. 964-981, 2023.

• BRAVO-MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNÁN D. ; CATALANO, FERNANDO M. . Potential Propulsive and Aerodynamic Benefits of a New Aircraft Concept: A Low-Speed Experimental Study. Aerospace , v. 10, p. 651, 2023.

• BRAVO-MOSQUERA, PEDRO D. ; CATALANO, FERNANDO M. ; ZINGG, DAVID W. . Unconventional aircraft for civil aviation: A review of concepts and design methodologies. PROGRESS IN AEROSPACE SCIENCES , v. 131, p. 100813, 2022.

• BRAVO-MOSQUERA, PEDRO D ; VACA-RIOS, JOHN J ; DIAZ-MOLINA, ANNY I ; AMAYA-OSPINA, MARÍA A ; CERÓN-MUÑOZ, HERNÁN D . Design and aerodynamic evaluation of a medium short takeoff and landing tactical transport aircraft. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING , v. 236, p. 825-841, 2022.

• BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN DARÍO ; CATALANO, FERNANDO MARTINI . Design, aerodynamic analysis and optimization of a next-generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering , v. 44, p. 609, 2022.

• GARCIA-RIBEIRO, DANIEL ; FLORES-MEZARINA, JUAN A. ; BRAVO-MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNAN D. . Parametric CFD analysis of the taper ratio effects of a winglet on the performance of a Horizontal Axis Wind Turbine. SUSTAINABLE ENERGY TECHNOLOGIES AND ASSESSMENTS AN INTERNATIONAL JOURNAL , v. 47, p. 101489, 2021.

• EGUEA, JOÃO PAULO ; BRAVO-MOSQUERA, PEDRO DAVID ; CATALANO, FERNANDO MARTINI . Camber morphing winglet influence on aircraft drag breakdown and tip vortex structure. AEROSPACE SCIENCE AND TECHNOLOGY , v. 119, p. 107148, 2021.

• BRAVO-MOSQUERA, PEDRO DAVID ; ABDALLA, ALVARO MARTINS ; CERÓN-MUÑOZ, HERNÁN DARÍO ; MARTINI CATALANO, FERNANDO . Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraft. AEROSPACE SCIENCE AND TECHNOLOGY , v. 86, p. 497-519, 2019.

• BRAVO-MOSQUERA, PEDRO DAVID ; CISNEROS-INSUASTI, NELSON DAVID ; MOSQUERA-RIVADENEIRA, FABIOLA ; AVENDAÑO-URIBE, BRYANN . STEM Learning Based on Aircraft Design: An Interdisciplinary Strategy Developed to Science Clubs Colombia. Ciencia y Poder Aéreo , v. 14, p. 204-227, 2019.

• BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN DARÍO ; DÍAZ-VÁZQUEZ, GUILLERMO ; MARTINI CATALANO, FERNANDO . Conceptual design and CFD analysis of a new prototype of agricultural aircraft. AEROSPACE SCIENCE AND TECHNOLOGY , v. 80, p. 156-176, 2018.

• BRAVO-MOSQUERA, PEDRO DAVID ; BOTERO-BOLIVAR, LAURA ; ACEVEDO-GIRALDO, DANIEL ; CERÓN-MUÑOZ, HERNÁN DARÍO . Aerodynamic design analysis of a UAV for superficial research of volcanic environments. AEROSPACE SCIENCE AND TECHNOLOGY , v. 70, p. 600-614, 2017.

• PEDRAZA BETANCOURTH, NELSON JAVIER ; PARRA VILLAMARIN, JULIO ENOC ; VACA RIOS, JOHN JAIRO ; BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN DARÍO . Design and Manufacture of a Solar-Powered Unmanned Aerial Vehicle for Civilian Surveillance Missions. JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT (ONLINE) , v. 8, p. 385-396, 2016.

• GONZALEZ DE GREIFF, PABLO ; GOMEZ RIVERA, WILLIAM ; BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN . Computational Analysis of the effect of Wavy Leading Edge on Stabilizer. In: 27^th Brazilian Congress of Thermal Sciences and Engineering, 2023. Proceedings of the 27th International Congress of Mechanical Engineering.

• ASSATO, M. ; INCEER, A. A. ; MORAES, L. ; TOMITA, J. T. ; BRINGHENTI, C. ; BRAVO-MOSQUERA, PEDRO D ; ROSELL, D. ; GRONSTEDT, T. . Performance benefits of a fan on blade ? flade ? for a variable cycle engine. In: 33rd Congress of the International Council of the Aeronautical Sciences, 2022, Stockholm. 33rd Congress of the International Council of the Aeronautical Sciences, 2022.

• ROSELL, D. ; GRONSTEDT, T. ; BRAVO-MOSQUERA, PEDRO DAVID ; CATALANO, FERNANDO . Low BPR turbofan performance with power extraction. In: 33rd Congress of the International Council of the Aeronautical Sciences, 2022, Stockholm. 33rd Congress of the International Council of the Aeronautical Sciences.

• BRAVO-MOSQUERA, PEDRO D. ; EGUEA, JOÃO PAULO ; CERÓN-MUÑOZ, HERNÁN D ; FERNANDO CATALANO . Experimental investigation of a next-generation airliner with boundary layer ingestion. In: 33rd Congress of the International Council of the Aeronautical Sciences, 2022, Stockholm. 33rd Congress of the International Council of the Aeronautical Sciences, 2022.

• BRAVO-MOSQUERA, PEDRO D. ; CHAU, T. ; CATALANO, FERNANDO M. ; ZINGG, DAVID W. . Exploration of Box-Wing Aircraft Concept Using High-Fidelity Aerodynamic Shape Optimization. In: 33rd Congress of the International Council of the Aeronautical Sciences, 2022. 33rd Congress of the International Council of the Aeronautical Sciences, 2022.

• FLOREZ, JUAN ; BRAVO MOSQUERA, PEDRO D. ; GARCIA RIBEIRO, DANIEL ; CERÓN MUNOZ, HERNÁN DARIO . Performance effects of winglets with leading edge protuberances on a rectangular wing. In: AIAA Scitech 2021 Forum, 2021, VIRTUAL EVENT. AIAA Scitech 2021 Forum, 2021.

• GARCIA RIBEIRO, DANIEL ; BRAVO MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNAN D. . Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In: AIAA Propulsion and Energy 2019 Forum, 2019, Indianapolis. AIAA Propulsion and Energy 2019 Forum. Reston: American Institute of Aeronautics and Astronautics, 2019.

• RIBEIRO, BRUNO ; BRAVO MOSQUERA, PEDRO D. ; CATALANO, FERNANDO . Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In: AIAA Propulsion and Energy 2019 Forum, 2019, Indianapolis. AIAA Propulsion and Energy 2019 Forum. Reston: American Institute of Aeronautics and Astronautics, 2019.

• BRAVO MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNAN D. ; CATALANO, FERNANDO . Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In: AIAA Propulsion and Energy 2019 Forum, 2019, Indianapolis. AIAA Propulsion and Energy 2019 Forum. Reston: American Institute of Aeronautics and Astronautics, 2019.

• GARCIA RIBEIRO, DANIEL ; FLORES MEZARINA, JUAN ; BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN ; VACA-RIOS, JOHN JAIRO . Side Force Coefficient Evaluation of a Commercial Bus with Vortex Generators. In: 25th International Congress of Mechanical Engineering, 2019. Proceedings of the 25th International Congress of Mechanical Engineering.

• FLORES MEZARINA, JUAN ; GARCIA RIBEIRO, DANIEL ; BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN . AERODYNAMIC EFFECTS OF ASYMMETRICAL LEADING EDGE PROTUBERANCES ON A RECTANGULAR WING. In: 25th International Congress of Mechanical Engineering, 2019. Proceedings of the 25th International Congress of Mechanical Engineering.

• Boccato, B ; BRAVO-MOSQUERA, PEDRO DAVID ; CATALANO, FERNANDO . ANÁLISE DOS EFEITOS AERODINÂMICOS DO CANARD EM UMA AERONAVE MILITAR NÃO CONVENCIONAL. In: 3o SiPGEM - 3o Simpósio do Programa de Pós-Graduação em Engenharia Mecânica, 2018, São Carlos. 3o SiPGEM - 3o Simpósio do Programa de Pós-Graduação em Engenharia Mecânica, 2018.

• BRAVO-MOSQUERA, PEDRO DAVID ; A. M. Abdalla ; CATALANO, FERNANDO . EVALUATION OF DELTA WING EFFECTS ON THE STEALTH-AERODYNAMIC FEATURES FOR NON-CONVENTIONAL FIGHTER AIRCRAFT. In: 31st Congress of International Council of the Aeronautical Sciences, 2018, Belo Horizonte. 31st Congress of International Council of the Aeronautical Sciences, 2018.

• BRAVO-MOSQUERA, PEDRO DAVID ; ÁLVARO MARTINS ABDALLA ; Cerón-Muñoz H D ; MARTINI CATALANO, FERNANDO . DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION. In: 31st Congress of International Council of the Aeronautical Sciences, 2018, Belo Horizonte. 31st Congress of International Council of the Aeronautical Sciences, 2018.

• BRAVO-MOSQUERA, PEDRO DAVID ; Botero, L ; ACEVEDO-GIRALDO, DANIEL ; CERÓN-MUÑOZ, HERNÁN DARÍO ; MARTINI CATALANO, FERNANDO . EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE. In: 31st Congress of International Council of the Aeronautical Sciences, 2018, Belo Horizonte. 31st Congress of International Council of the Aeronautical Sciences, 2018.

• Garcia, D ; CERÓN-MUÑOZ, HERNÁN ; BRAVO-MOSQUERA, PEDRO DAVID . Aerodynamic Heating Effect on Roughness, Aerodynamic Coefficients and Power Output of Aerogenerators - a Discussion. In: 17th Brazilian Congress of Thermal Sciences and Engineering, 2018, Águas de Lindóia. 17th Brazilian Congress of Thermal Sciences and Engineering, 2018.

• ACEVEDO-GIRALDO, DANIEL ; BOTERO-BOLIVAR, LAURA ; BRAVO-MOSQUERA, PEDRO DAVID ; CERÓN-MUÑOZ, HERNÁN ; CATALANO, FERNANDO . EXPERIMENTAL ASSESMENT OF A LOW REYNOLDS NUMBER VEHICLE. In: 24th ABCM International Congress of Mechanical Engineering, 2017, Curitiba. Procceedings of the 24th ABCM International Congress of Mechanical Engineering, 2017.

• Bravo-Mosquera, P. D ; Cerón-Muñoz H D ; F.M. Catalano . ANALYTICAL AND NUMERICAL DESIGN OF A MIXED-COMPRESSION AIR INTAKE FOR A SUPERSONIC AIRCRAFT. In: 1o SiPGEM - 1o Simpósio do Programa de Pós-Graduação em Engenharia Mecânica, 2016, São Carlos. 1o SiPGEM - 1o Simpósio do Programa de Pós-Graduação em Engenharia Mecânica, 2016. v. 1.

• Bravo-Mosquera, P. D ; A. M. Abdalla ; Cerón-Muñoz H D ; F.M. Catalano . CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING. In: 30th Congress of the International Council of the Aeronautical Science, 2016, Daejeon. ICAS 2016, 2016. v. 30.

• Cerón-Muñoz H D ; Diaz D ; Bravo-Mosquera, P. D ; F.M. Catalano ; Santana L D . EXPERIMENTAL ANALYSES OF DROOP, WINGTIPSAND FENCES ON A BWB MODEL. In: 30th Congress of the International Council of the Aeronautical Science, 2016, Daejeon. ICAS 2016, 2016. v. 30.

• Bravo-Mosquera, P. D ; A. M. Abdalla ; Cerón-Muñoz H D ; F.M. Catalano . AERODYNAMIC ANALYSIS OF THE INFLUENCE OF CANOPY SHAPE IN THE SUPERSONIC DORSAL INTAKE DESIGN. In: Aerospace Technology Congress 2016, 2016, Stockholm. Aerospace Technology Congress 2016, 2016.

• PEDRO DAVID BRAVO MOSQUERA ; ÁLVARO URIBE AGUDELO ; FERNANDO CATALANO ; ÁLVARO MARTINS ABDALLA . Parametric Conceptual Design of a UAV for Superficial Volcano Monitoring.. In: 23rd ABCM International Congress of Mechanical Engineering, 2015, Rio de Janeiro. v. 23.

• Cerón-Muñoz H D ; Diaz D ; BRAVO-MOSQUERA, PEDRO DAVID ; CATALANO, FERNANDO . Wind Tunnel Experiments of Winglet, C-wing and Fences coupled to a ?Blended Wing Body? Model. In: Aerospace Technology Congress 2016, 2016. Aerospace Technology Congress 2016, 2016.

• BRAVO-MOSQUERA, PEDRO D. ; CHAU, T. ; CATALANO, FERNANDO ; ZINGG, DAVID W. . Exploration of box-wing aircraft concept using high-fidelity aerodynamic shape optimization. 2022. (Apresentação de Trabalho/Congresso).

• BRAVO-MOSQUERA, PEDRO DAVID ; VACA RIOS, JOHN JAIRO . DISEÑO CONCEPTUAL DE UNA AERONAVE DE TRANSPORTE TÁCTICO TIPO STOL. 2019. (Apresentação de Trabalho/Comunicação).

• BRAVO-MOSQUERA, PEDRO D. ; CERÓN-MUÑOZ, HERNÁN D ; CATALANO, FERNANDO . Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019. (Apresentação de Trabalho/Congresso).

• MOSQUERA, P. D. B. ; Cerón-Muñoz H D ; F.M. Catalano . Analytical and Numerical Design of a Mixed-Compression Air Intake For a Supersonic Fighter Aircraft. 2016. (Apresentação de Trabalho/Simpósio).

• Bravo-Mosquera, P. D ; ÁLVARO URIBE AGUDELO ; A. M. Abdalla ; MARTINI CATALANO, FERNANDO . Parametric Conceptual Design of a UAV for Superficial Volcano Monitoring. 2015. (Apresentação de Trabalho/Congresso).

• MOSQUERA, P. D. B. . Pensamiento Cuántico y Teoría de Cuerdas. 2009. (Apresentação de Trabalho/Conferência ou palestra).

Outras produções

Projetos de pesquisa

• 2018 - 2020

  Design, aerodynamic evaluation and optimization of a medium STOL tactical transport aircraft, Descrição: This project deals with the conceptual design and optimization of a medium STOL (Short Take-off and Landing) tactical transport aircraft, which is intended to expand the institutional capabilities of the Colombian Air Force (FAC) in terms of versatility and flexibility. A multifidelity design strategy was developed during the conceptual design stage of the aircraft, combining classical methodologies and high-fidelity Computational Fluid Dynamics (CFD) simulations. This methodology allowed the aircraft to be assessed in a single design space, based on its design requirements, mission and applicable airworthiness standards. The optimized aircraft is compared to major competitors in order to discuss and highlight its main advantages and feasibility for future production.. , Situação: Concluído; Natureza: Pesquisa. , Alunos envolvidos: Graduação: (8) / Mestrado acadêmico: (1) / Doutorado: (1) . , Integrantes: Pedro David Bravo Mosquera - Coordenador / VACA RIOS, JOHN JAIRO - Integrante.

• 2017 - 2022

  Multidisciplinary design optimization of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system, Descrição: Nowadays, due to technological evolution as well as several green aerospace projects, the aeronautical community is implementing advanced design strategies looking for the next future airliner configuration. The use of significant technology breakthroughs in the area of aircraft design allows the identification of large-scale aerodynamic data to understand the aircraft performance and its implication to mitigate the undesirable impact of airliners on the environment. In order to achieve ambitious goals, non-conventional solutions have attracted the attention of designers, highlighting the closed non-planar wing configurations, which have shown a reduction in pollutant emissions by minimizing the induced drag, in addition to presenting several advantages when compared to conventional designs, such as a reduced empty weight and a better aerodynamic efficiency. Likewise, boundary layer ingestion (BLI) has emerged as a potential propulsion concept for future aircraft configurations, mainly by reducing wasted kinetic energy in the exhaust jet, due to the lower wake velocities obtained by the combination of the aircraft wake along with the propulsor jet, thus reducing cruise energy consumption and CO2 emissions. Based on the aforementioned approaches, this investigation intends to combine the potential benefits of a closed-wing configuration with a BLI propulsion system in order to develop a modern and advanced civil transport aircraft. During the conceptual design phase, a novel computer-based design method is developed in order to determine the main geometric, aerodynamic, stability and performance characteristics of the aircraft, based on its design requirements and constraints. Once obtained a baseline concept, a scale-model will be manufactured in order to perform a back-to-back wind-tunnel analysis of non-boundary layer ingesting and boundary layer ingesting versions of the aircraft. Finally, the aerodynamic design optimization will take place through a computational fluid dynamics (CFD) formulation, using continuous adjoint methods and incorporating a gradient-based optimizer. It is expected that such data will be useful in interpreting that a closed-wing aircraft coupled to a BLI propulsion system can meet the demands of future aviation.. , Situação: Concluído; Natureza: Pesquisa. , Alunos envolvidos: Doutorado: (2) . , Integrantes: Pedro David Bravo Mosquera - Coordenador / MARTINI CATALANO, FERNANDO - Integrante., Financiador(es): Conselho Nacional de Desenvolvimento Científico e Tecnológico - Bolsa.

• 2015 - 2017

  Multidisciplinary Optimization and Aerodynamic Design of an Air Intake System for a Non-conventional Fighter Aircraft, Descrição: The conception of non-conventional aircraft to achieve a certain performance or operational improvement is undoubtedly, one of the most important objectives of the aeronautical engineering. This work presents the conceptual design and the intake aerodynamic analysis of a non-conventional aircraft whose main design feature is an inverted-rectangular dorsal intake with external compression, followed by a three dimensional transitioning S-duct diffuser with circular cross section at aerodynamic interface plane. An in-house presizing tool was developed to define the key layout characteristics and select the optimal airframe-engine combination regarding the design requirements of the aircraft, whereas Reynolds-averaged Navier-Stokes (RANS) simulations were also conducted to assess the performance of the intake-airframe integration at several flight conditions. The results found in this work were evaluated separately. First, the analytic design method of the intake itself was compared with numerical simulations in order to check and maximize the total pressure recovery at on-design condition. Subsequently, the intake-airframe integration assessment took place, showing that adequate performance and compatibility characteristics are maintained during subsonic and transonic maneuvers. However, at supersonic velocities, the flow expansion on the fuselage and wings produced an increase in the local Mach number which reduce the intake performance levels. These studies provided an extensive data to evaluate the effects of specific aircraft design variables on dorsal intake performance, such as the integration of the cockpit, the boundary layer diverter, and several delta wing configurations. All numerical results show that, dorsal intakes are a promising alternative for aircraft that require only reasonable supersonic maneuverability capabilities and high subsonic and transonic capabilities. In addition, dorsal intake coupled to S-duct diffuser provide line-of-sight blockage of the engine blades, satisfying the requirement of low radar signature, lightweight and low drag of the next generation of fighter aircraft.. , Situação: Concluído; Natureza: Pesquisa. , Alunos envolvidos: Doutorado: (3) . , Integrantes: Pedro David Bravo Mosquera - Coordenador / Fernando Catalano - Integrante / Alvaro Abdalla - Integrante.

• 2014 - 2017

  Conceptual and Preliminary Design of a UAV for Superficial Volcano Monitoring, Descrição: When volcanoes manifest unusual signs of activity, real-time data aids for evaluating and communicating reports about volcanic hazards. For this reason, the present research aims the aerodynamic design of a low-cost unmanned aerial vehicle (UAV) able to perform aerial surveillance of volcanic environments. Its main mission is to transmit real-time volcanic data to a remote location, in order to aid to forecast volcanic eruptions, as well as avoiding the exposition of pilots and scientists to these dangerous flight conditions. During the conceptual design phase, classical and new design procedures were developed in order to determine the vehicle design requirements, in relation to its flight in a hard scenario like an active volcano. Likewise, the main geometric, aerodynamic, stability and performance parameters of the UAV were calculated and assessed through theoretical/analytical presizing and Computer-aided Design (CAD) methods. After obtaining the final concept, the aerodynamic design was carried out considering the constraints found in the previous design phase. In this way, an accurate estimation of the aerodynamic coefficients was developed, through analytical simulations, Computational Fluid Dynamics (CFD) simulations and wind tunnel testing. Results showed that the entire design process was consistent because the analytical, numerical and experimental results were greatly similar in the Lift and Drag coefficients. Furthermore, the UAV characteristics are within the limits of the design requirements, presenting several aerodynamic and performance advantages in comparison to other vehicles used in the same mission. This suggested that, on a large scale, the aerodynamic behavior of the UAV is suitable for performing the mission for which it was created. However, actual-environmental studies are still necessary in order to validate the reliability of the designed UAV.. , Situação: Concluído; Natureza: Pesquisa. , Alunos envolvidos: Graduação: (2) / Mestrado acadêmico: (1) / Doutorado: (1) . , Integrantes: Pedro David Bravo Mosquera - Coordenador / Hernán Darío Cerón Muñoz - Integrante.

Prêmios