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Jose Nivaldo Hinckel
Jose Nivaldo Hinckel
Chefe de Pesquisa e Desenvolvimento, Fibraforte Engenharia Indústria e Comércio
Geverifieerd e-mailadres voor fibraforte.com.br
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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
772004
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
172009
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
122018
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
102001
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
101986
CFD analysis of swirl atomizers
JN Hinckel, HF Villa Nova, VG Bazarov
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008
72008
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
62000
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
51999
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
51991
EXPERIMENTAL STUDY OF THE HEAT TRANSFER RATE IN THE JUNCTION REGION OF A CIRCULAR CYLINDER PERPENDICULAR TO A FLAT PLATE.
JN Hinckel
51985
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
42018
CFD Analysis of Swirl Atomizers
V Bazarov, J Hinckel, H Villa Nova
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5229, 2012
32012
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
31998
An object oriented approach to launch vehicle performance analysis
J Hinckel
31st Joint Propulsion Conference and Exhibit, 3094, 1995
31995
Development of a 115 newton thrust hydrazine catalytic thruster
J HINCKEL
29th Joint Propulsion Conference and Exhibit, 1964, 1993
21993
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
12020
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
12019
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
12015
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
12011
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
12005
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Artikelen 1–20