Numerical solutions of flows in rocket engines with regenerative cooling CH Marchi, F Laroca, AFC Silva, JN Hinckel Numerical Heat Transfer, Part A: Applications 45 (7), 699-717, 2004 | 77 | 2004 |
Low cost catalysts for hydrazine monopropellant thrusters J Hinckel, J Jorge, T Soares, M Zacharias, J Palandi 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5232, 2009 | 17 | 2009 |
Modeling and analysis of a LOX/Ethanol liquid rocket engine FAS Mota, JN Hinckel, EM Rocco, H Schlingloff Journal of Aerospace Technology and Management 10, e3018, 2018 | 12 | 2018 |
Organization of the working process in the small thrust engine LRESTh MAI-200 AA Kozlov, VM Abashev, JN Hinckel 52-nd International Astronautical Congress (October 1–5, 2001) Toulouse, France, 2001 | 10 | 2001 |
Heat transfer in the stagnation region of the junction of a circular cylinder perpendicular to a flat plate JN Hinckel, HT Nagamatsu International journal of heat and mass transfer 29 (7), 999-1005, 1986 | 10 | 1986 |
CFD analysis of swirl atomizers JN Hinckel, HF Villa Nova, VG Bazarov 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008 | 7 | 2008 |
Solução numérica de escoamentos em motor-foguete com refrigeração regenerativa CH Marchi, F Laroca, AFC Silva, JN Hinckel XXI Iberian Latin American Congress on Computational Methods in Engineering …, 2000 | 6 | 2000 |
Payload evaluation of a tripropellant carrier rocket AA Kozlov, JN Hinckel, J Koreeda, A Comiran Journal of propulsion and power 15 (2), 304-309, 1999 | 5 | 1999 |
Propulsion subsystem component development program for the MECB RSS Satellite J HINCKEL, V TRAVA-AIROLDI, E CORAT, C BRESSAN 27th Joint Propulsion Conference, 1836, 1991 | 5 | 1991 |
EXPERIMENTAL STUDY OF THE HEAT TRANSFER RATE IN THE JUNCTION REGION OF A CIRCULAR CYLINDER PERPENDICULAR TO A FLAT PLATE. JN Hinckel | 5 | 1985 |
Trajectory Optimization of Launch Vehicles Using Object-oriented Programming FAS Mota, JN Hinckel, EM Rocco, H Schlingloff Journal of aerospace technology and management 10, e3918, 2018 | 4 | 2018 |
CFD Analysis of Swirl Atomizers V Bazarov, J Hinckel, H Villa Nova 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5229, 2012 | 3 | 2012 |
Controlled porosity carbides used as hydrazine decomposition catalysts J Gobbo-Ferreira, J Rodrigues, J Hinckel, C Migueis, G DaCruz 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3995, 1998 | 3 | 1998 |
An object oriented approach to launch vehicle performance analysis J Hinckel 31st Joint Propulsion Conference and Exhibit, 3094, 1995 | 3 | 1995 |
Development of a 115 newton thrust hydrazine catalytic thruster J HINCKEL 29th Joint Propulsion Conference and Exhibit, 1964, 1993 | 2 | 1993 |
DESIGN AND TEST OF NON-UNIFORM SPRAY SWIRL INJECTORS AND ITS APPLICATIONS IN INJECTION PLATE DESIGN A Goulart, J Hinckel, L Bontempo 71st International Astronautical Congress (IAC)–The CyberSpace Edition, 12-14, 2020 | 1 | 2020 |
Modulation of the Spray Jet of a Swirl Injector JN Hinckel, AC Goulart, LP Bontempo, ... Proceedings of the 8th European Conference for Aeronautics and Space …, 2019 | 1 | 2019 |
Modeling and Simulation of Launch Vehicles Using Object-Oriented Programming: Impact of the Engine Parameters on the Launcher Performance FA Mota, JN Hinckel, EM Rocco, H Schlingloff, JN Hinckel Proceedings of the 6th European Conference for Aeronautics and Space …, 2015 | 1 | 2015 |
GEO+ ES Hybrid Optimization Algorithm Applied to the Parametric Thermal Model Estimation of a 200N Hydrazine Thruster RL Galski, H Patire Ju´ nior, FL de Sousa, JN Hinckel, P Lacava, ... International Design Engineering Technical Conferences and Computers and …, 2011 | 1 | 2011 |
Analysis of the Flow in Liquid Propellant Engine Swirl Injectors Using CFD JEC Infantes, JN Hinckel Proceedings of the COBEM 2005: 18 th International Congress of Mechanical …, 2005 | 1 | 2005 |