- 121. Mathematical modeling of transient processes during startup of main liquid propellant engine under hot test conditions - Dmytro Koptilyy, Roman Marchan, Sergey Dolgopolov and Olexiy Nikolayev FireFly Aerospace ...
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- DOI: 10.13009/EUCASS2019-236 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Mathematical modeling of transient processes during startup of main liquid propellant engine under hot ...
- 122. 3D printed acoustic igniter of oxygen-kerosene mixtures for aerospace applications - Roman Marchan*, Andrii Oleshchenko**, Samir Vekilov***, Mihaylo Arsenuk**** and Olexander Bobrov***** *Firefly Aerospace ...
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- DOI: 10.13009/EUCASS2019-238 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 3D printed acoustic igniter of oxygen-kerosene mixtures for aerospace applications Roman Marchan*, Andrii ...
- 123. The Influence of Meteorological Conditions on the Icing Performance Penalties on a UAV Airfoil - Nicolas Fajt*, Richard Hann* and Thorsten Lutz** *Norwegian University of Science and Technology, 7034 Trondheim, ...
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- DOI: 10.13009/EUCASS2019-240 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The Influence of Meteorological Conditions on the Icing Performance Penalties on a UAV Airfoil Nicolas ...
- 124. Integrated Navigation using MEMS-based Inertial, GPS and Sun Vector Measurements aboard the Spin-Stabilized PMWE-1 Sounding Rocket - Benjamin Braun*, Jochen Barf**, Markus Markgraf*** German Aerospace ...
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- DOI: 10.13009/EUCASS2019-241 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Integrated Navigation using MEMS-based Inertial, GPS and Sun Vector Measurements aboard the Spin-Stabilized ...
- 125. Novel gelled fuels containing nanoparticles as hypergolic bipropellants with HTP - Sophie Ricker1*2, Maxim Kurilov1, Dominic Freudenmann1, Christoph Kirchberger1, Tobias Hertel2, Helmut Ciezki1 and Stefan ...
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- DOI: 10.13009/EUCASS2019-242 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Novel gelled fuels containing nanoparticles as hypergolic bipropellants with HTP Sophie Ricker1*2, Maxim ...
- 126. Launcher Vehicle Aerothermodynamics and Fairing Separation Altitude E?ects on Payload Temperature - Alessandro Falchi,† Lorenzo Gentile, Edmondo Minisci Aerospace Centre of Excellence, University of S
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- DOI: 10.13009/EUCASS2019-243 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Launcher Vehicle Aerothermodynamics and Fairing Separation Altitude E?ects ...
- 127. Optimization of the base bleed to control trailing edge ?ows in a wide range of Mach numbers - Alejandro Martinez-Cava1† , Eusebio Valero1 , Jorge Saavedra2 , Francisco Lozano2 and Guillermo Paniagua2 ...
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- DOI: 10.13009/EUCASS2019-244 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Optimization of the base bleed to control trailing edge ?ows in a wide range of Mach numbers Alejandro ...
- 128. Effects of Cavities on Pressure Fluctuation Characteristics of Hypersonic Vehicle Wall Plate - Haiyan Li*, Xing Chen**,Hongbo Lu ,Jian Lin, Nong Chen, *China Academy of Aerospace Aerodynamics, 17 Yungang ...
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- DOI: 10.13009/EUCASS2019-246 Effects of Cavities on Pressure Fluctuation Characteristics of Hypersonic Vehicle Wall Plate Haiyan Li*, Xing Chen**,Hongbo Lu ,Jian Lin, Nong Chen, *China Academy of Aerospace ...
- 129. Experimental Study on Thermal Decomposition of Several Kerosene Fuels - Donghyun Hwang*, Bom Lee**, and Kyubok Ahn*** *School of Mechanical Engineering, Chungbuk National University 1 Chungdae-ro, Seowon-gu, ...
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- DOI: 10.13009/EUCASS2019-247 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental Study on Thermal Decomposition of Several Kerosene Fuels Donghyun Hwang*, Bom Lee**, and Kyubok ...
- 130. Derivation of Buckling Knockdown Factors Using The Equivalent Model for Isogrid-Stiffened Cylinders - Han-Il Kim1*, Chang-Hoon Sim2*, Jae-Sang Park3*, Keejoo Lee4§, Joon-Tae Yoo5§, and Young-Ha Yoon6§ ...
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- DOI: 10.13009/EUCASS2019-248 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Derivation of Buckling Knockdown Factors Using The Equivalent Model for Isogrid-Stiffened Cylinders Han-Il ...
- 131. 3D ...
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- DOI: 10.13009/EUCASS2019-251 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE 3D Conjugate Heat Transfer Analysis of a 100 kN Class Liquid Rocket Combustion ...
- 132. Wall-Modeled Large Eddy Simulation for Predicting Wall Heat Flux in a Rocket Combustion Chamber - Daiki Muto? , Yu Daimon?? , Taro Shimizu? , and Hideyo Negishi?? ? Japan Aerospace Exploration Agency 3-1-1 ...
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- DOI: 10.13009/EUCASS2019-252 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Wall-Modeled Large Eddy Simulation for Predicting Wall Heat Flux in a Rocket Combustion Chamber Daiki ...
- 133. Combined experimental and calculation method for sonic boom investigation - Tatiana Kiseleva* * Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of Russian Academy of Sciences, ...
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- DOI: 10.13009/EUCASS2019-254 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Combined experimental and calculation method for sonic boom investigation Tatiana Kiseleva* * Khristianovich ...
- 134. Characterization under Uncertainty of Catalytic Phenomena in Ceramic Matrix Composites Materials for Spacecraft Thermal Protection Systems - Diana Luís1,† , Anabel del Val1,2,† and Olivier Chazot1 1 von ...
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- DOI: 10.13009/EUCASS2019-257 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: Characterization under Uncertainty of Catalytic Phenomena in Ceramic Matrix Composites Materials ...
- 135. Fragmentation and formation of the condensed products during combustion of titanium particles in air - Belousova N. S.*, Glotov O. G.**, Surodin G. S.*** * Voevodsky Institute of Chemical Kinetics and ...
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- DOI: 10.13009/EUCASS2019-258 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Fragmentation and formation of the condensed products during combustion of titanium particles in air Belousova ...
- 136. Near-field sonic boom signature measurement system for AVIC ARI’s FL-60 wind tunnel - Liu Zhongchen 1, 2, Qian Zhansen 1, 2,*, Leng Yan 1, 2 1. AVIC Aerodynamics Research Institute, Shenyang, 110034, China ...
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- DOI: 10.13009/EUCASS2019-259 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Near-field sonic boom signature measurement system for AVIC ARI’s FL-60 wind tunnel Liu Zhongchen 1, 2, ...
- 137. Combustion characteristics of model composite propellants containing boron and its compounds - Glotov O. G.*, Yagodnikov D. A.**, Kiskin A. B.***, Surodin G. S.**** * Voevodsky Institute of Chemical Kinetics ...
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- DOI: 10.13009/EUCASS2019-260 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Combustion characteristics of model composite propellants containing boron and its compounds Glotov O. ...
- 138. Some aspects of transonic flutter of aircraft with laminar wings - S. Kuzmina*, F. Ishmuratov**, O. Karas*** *Leading research scientist, Central Aerohydrodynamic Institute (TsAGI) e-mail: kuzmina@tsagi.ru ...
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- DOI: 10.13009/EUCASS2019-261 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Some aspects of transonic flutter of aircraft with laminar wings S. Kuzmina*, F. Ishmuratov**, O. Karas*** ...
- 139. Reusable Structures for CALLISTO - Sofia Giagkozoglou Vincenzino* and Waldemar Rotärmel*, Ivaylo Petkov*, Henning Elsäßer*, Etienne Dumont**, Lars Witte **, Silvio Schröder** * DLR, Institute of Structures ...
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- DOI: 10.13009/EUCASS2019-262 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Reusable Structures for CALLISTO Sofia Giagkozoglou Vincenzino* and Waldemar Rotärmel*, Ivaylo Petkov*, ...
- 140. Numerically E?cient Fatigue Life Prediction of Rocket Combustion Chambers using Arti?cial Neural Networks - Kai Dresia† , Günther Waxenegger-Wil?ng, Jörg Riccius, Jan Deeken and Michael Oschwald German ...
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- DOI: 10.13009/EUCASS2019-264 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: 264 Numerically E?cient Fatigue Life Prediction of Rocket Combustion Chambers using Arti?cial ...