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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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 ...
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, ...
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. ...
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*** ...
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*, ...
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 ...