- 281. Development of Computational and Experimental Methods for Determining Dynamic Characteristics of Aircraft Landing Gear - E. S. Kolyshev1, A.V. Krapivko2
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- DOI: 10.13009/EUCASS2019-502 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Development of Computational and Experimental Methods for Determining Dynamic Characteristics of Aircraft ...
- 282. Role of combustion modeling in the prediction of heat transfer in LRE thrust chambers - F. Nasuti ?, P. Concio , G. Indelicato , P.E. Lapenna and F. Creta Sapienza University of Rome Dipartimento di Ingegneria ...
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- DOI: 10.13009/EUCASS2019-503 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Role of combustion modeling in the prediction of heat transfer in LRE thrust ...
- 283. Computational Design of a CubeSat Compatible Re-entry Capsule - Mohammad Yousefi* and Cliff Wachiuri** and Vishva Plaitharathna*** and Mahmoud Hamdy**** and Boutheina Tlili***** and Mihail Barbosu****** ...
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- DOI: 10.13009/EUCASS2019-504 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Computational Design of a CubeSat Compatible Re-entry Capsule Mohammad Yousefi* and Cliff Wachiuri** and ...
- 284. Three-dimensional adaptive neural network guidance law against maneuvering targets - Si Yujie1*, Xiong Hua1, Xiong Shaofeng1 1 Beijing Institute of Electronic System Engineering, 100854, People?s Republic ...
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- DOI: 10.13009/EUCASS2019-505 Three-dimensional adaptive neural network guidance law against maneuvering targets Si Yujie1*, Xiong Hua1, Xiong Shaofeng1 1 Beijing Institute of Electronic System Engineering, ...
- 285. Application of hybrid numerical schemes in prediction of high-speed laminar-turbulent transition - Ivan V. Egorov * and Can Nguyen** *Central Aerohydrodynamic Institute 1 Zhukovsky st., Zhukovsky, Moscow ...
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- DOI: 10.13009/EUCASS2019-507 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Application of hybrid numerical schemes in prediction of high-speed laminar-turbulent transition Ivan V. ...
- 286. Development of new analytical models for pressure and heat ?ux distributions on space debris afterbodies - Vincent Drouet ? , Ysolde Pr?vereaud , Jean-Marc Moschetta? ONERA ONERA Toulouse Center, 2 avenue ...
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- DOI: 10.13009/EUCASS2019-508 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Development of new analytical models for pressure and heat ?ux distributions ...
- 287. Lithium-sulphur batteries: opportunities and challenges for space applications - G?raldine Palissat*
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- DOI: 10.13009/EUCASS2019-509 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Lithium-sulphur batteries: opportunities and challenges for space applications G?raldine Palissat* *ArianeGroup 51?61 ...
- 288. Design of the trajectory of a tether mission to Saturn - Riccardo Calaon? , Elena Fantino?, Roberto Flores ? and Jes?s Pel?ez? ? Dept. of Industrial Engineering, University of Padova Via Gradenigio G/a ...
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- DOI: 10.13009/EUCASS2019-510 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: Design of the trajectory of a tether mission to Saturn Riccardo Calaon? , Elena Fantino?, Roberto ...
- 289. A Timescale-Augmented Spalart-Allmaras Turbulence Model for Flamelet Combustion Applications - Tim Horchler? , Stefan Fechter, Sebastian Karl and Klaus Hannemann German Aerospace Center (DLR) Institute ...
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- DOI: 10.13009/EUCASS2019-512 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE A Timescale-Augmented Spalart-Allmaras Turbulence Model for Flamelet Combustion ...
- 290. Experimental Study on Jet Acoustics of Subscale Rocket Nozzles with a Different Divergent Contour Design - Ralf Stark, Dirk Schneider, Jan Martin and Stephan General German Aerospace Center Langer Grund, ...
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- DOI: 10.13009/EUCASS2019-514 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental Study on Jet Acoustics of Subscale Rocket Nozzles with a Different Divergent Contour Design Ralf ...
- 291. DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation - Dirk Schneider? , Justin Hardi, Jan Martin, Ralf Stark, Dmitry Suslov, Federica Tonti, Jan van Schyndel, Victor Zhukov and Michael Oschwald ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-515 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation Dirk Schneider? , Justin Hardi, Jan Martin, ...
- 292. Experimental Flow Path Analysis of a Hydrogen Transpiration Cooled Model Scramjet Combustor - Friedolin Strauss*, Stephan General*, Chiara Manfletti** and Stefan Schlechtriem* * German Aerospace Center ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-516 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental Flow Path Analysis of a Hydrogen Transpiration Cooled Model Scramjet Combustor Friedolin Strauss*, ...
- 293. NEMS and MEMS technologies in RLV maintenance operations - Massimo FERLIN*, Michal KURELA** Olivier LEHMANN*** *CNES Launcher Directorate Innovation Launcher System Paris-France Massimo.ferlin@cnes.fr ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-517 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) NEMS and MEMS technologies in RLV maintenance operations Massimo FERLIN*, Michal KURELA** Olivier LEHMANN*** ...
- 294. Smart Operations in ATEX RLV Environment - Massimo FERLIN*, Michal KURELA** Olivier MONGE and Christophe CASTGNET*** *CNES Launcher Directorate Innovation Launcher System Paris-France Massimo.ferlin@cnes.fr ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-518 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Smart Operations in ATEX RLV Environment Massimo FERLIN*, Michal KURELA** Olivier MONGE and Christophe ...
- 295. Reynolds number in?uence on the hysteresis behavior of a dual-bell nozzle - Alexander Barklage ? , Simon Loosen? , Wolfgang Schr?der? and Rolf Radespiel Institute of Fluid Mechanics, TU Braunschweig, Hermann-Blenk ...
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- DOI: 10.13009/EUCASS2019-519 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Reynolds number in?uence on the hysteresis behavior of a dual-bell nozzle Alexander ...
- 296. Development of a Reliable Performance Gas Generator of 75 tonf-class Liquid Rocket Engine for the Korea Space Launch Vehicle II - Byoungjik Lim*, Munki Kim*, Donghyuk Kang*, Hyeon-Jun Kim*, Jong-Gyu Kim*, ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-521 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Development of a Reliable Performance Gas Generator of 75 tonf-class Liquid Rocket Engine for the Korea ...
- 297. Numerical Simulation of Instabilities Evolution in a High-Speed Boundary Layer with Cross?ow Jet Injection - Andrey V. Novikov , and Alexander V. Fedorov , Central Aerohydrodynamic Institute (TsAGI) 1 ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-522 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Numerical Simulation of Instabilities Evolution in a High-Speed Boundary Layer with Cross?ow Jet Injection Andrey ...
- 298. Definition of a Configuration Module for a Concurrent Design Facility - Jos? Miguel ?lvarez Romero and Elena Roib?s-Mill?n Instituto Universitario de Microgravedad ?Ignacio da Riva?, Universidad Polit?cnica ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-525 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Definition of a Configuration Module for a Concurrent Design Facility Jos? Miguel ?lvarez Romero and Elena ...
- 299. Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application - R. H. S. Hahn*1, I. D. Hoffmann1, J. Deeken1, M. Oschwald1, S. Schlechtriem1 1 German Aerospace Center DLR, Institute ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-528 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application R. H. S. Hahn*1, ...
- 300. Experimental Study of the Natural Disturbance Evolution in a Swept Wing Boundary Layer with Periodic Spanwise Roughness at Mach 2 and 2.5 - Alexander Kosinov*, Nikolai Semionov**, Alexandra Panina, Gleb ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-530 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental Study of the Natural Disturbance Evolution in a Swept Wing Boundary Layer with Periodic Spanwise ...