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141. Composite Optimization Techniques for Aircraft Components Structural Sizing - José Carlos Martín Airbus Defence and Space Paseo John Lennon, 2, CP 28906, Getafe (Madrid)
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DOI: 10.13009/EUCASS2019-268 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Composite Optimization Techniques for Aircraft Components Structural Sizing José Carlos Martín Airbus Defence ...
142. A Sliding Mode Control in a Backstepping Setup for Rendezvous Mission on a Circular Orbit - Zenteno Torres Jazmín † , Cieslak Jérôme† , Henry David†,‡ , Dávila Jorge : IMS lab., Univ. Bordeaux, Bordeaux ...
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DOI: 10.13009/EUCASS2019-269 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE A Sliding Mode Control in a Backstepping Setup for Rendezvous Mission on a ...
143. 3D Printed Control Surface for UAVs - José Carlos Martín Airbus Defence and Space Paseo John Lennon, 2, CP 28906, Getafe (Madrid) Juan Miguel Abellán Airbus Defence and Space Paseo John Lennon, 2, CP 28906, ...
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DOI: 10.13009/EUCASS2019-270 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 3D Printed Control Surface for UAVs José Carlos Martín Airbus Defence and Space Paseo John Lennon, 2, CP ...
144. ZDES of an Ariane 6 PPH con?guration with incidence angle using Zonal Immersed Boundary Conditions - P. E. Weiss ONERA - The French Aerospace Lab, F-92190, Meudon, France
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DOI: 10.13009/EUCASS2019-274 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE ZDES of an Ariane 6 PPH con?guration with incidence angle using Zonal Immersed ...
145. New Control Functionalities for Launcher Load Relief in Ascent and Descent Flight* - Pedro Simplício †, Andrés Marcos and Samir Bennani Technology for Aerospace Control Lab, University of Bristol University ...
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DOI: 10.13009/EUCASS2019-275 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) New Control Functionalities for Launcher Load Relief in Ascent and Descent Flight* Pedro Simplício ...
146. Advanced Propellants for Space Propulsion – A Task within the DLR Interdisciplinary Project "Future Fuels" - Helmut K. Ciezki*1, Victor Zhukov*, Lukas Werling*, Christoph Kirchberger*, Clemens Naumann#, ...
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DOI: 10.13009/EUCASS2019-276 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Advanced Propellants for Space Propulsion – A Task within the DLR Interdisciplinary Project "Future Fuels" Helmut ...
147. Atomization and combustion of a single unlike-triplet spray of storable bipropellants: hydrogen peroxide with ethanol or alkanes - N. Riaud*, B. Boust* and M. Bellenoue* PPrime Institute, CNRS – ISAE-ENSMA ...
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DOI: 10.13009/EUCASS2019-279 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Atomization and combustion of a single unlike-triplet spray of storable bipropellants: hydrogen peroxide ...
148. Development of a Bonded Eurofighter Airbrake Flight Demonstrator - Mircea Calomfirescu*, Rainer Neumaier*, Anton Maier*, Thomas Körwien*, Helmut Thanhofer*, Thomas Meer**, Michael Hanke***, Sarah Froese ...
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DOI: 10.13009/EUCASS2019-280 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Development of a Bonded Eurofighter Airbrake Flight Demonstrator Mircea Calomfirescu*, Rainer Neumaier*, ...
149. Filter design using an iterative Hilbert transform scheme - Philippe SAUNOIS* *ArianeGroup, Les Mureaux, France Email: philippe.saunois@ariane.group
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DOI: 10.13009/EUCASS2019-282 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Filter design using an iterative Hilbert transform scheme Philippe SAUNOIS* *ArianeGroup, Les Mureaux, ...
150. Modeling and Control of Propellant Slosh Dynamics in Observation Spacecraft with Actuator Saturations - BOURDELLE Anthony 1† , BIANNIC Jean-Marc 1 , EVAIN Helene 2 PITTET Christelle 2 , MORENO Sabine 2 ...
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DOI: 10.13009/EUCASS2019-283 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Modeling and Control of Propellant Slosh Dynamics in Observation Spacecraft with Actuator Saturations BOURDELLE ...
151. Guidance and Control Strategy for the CALLISTO Flight Experiment - Marco Sagliano † , Taro Tsukamoto† , José A. Macés-Hernández , David Seelbinder , Shinji Ishimoto† , Etienne Dumont , † DLR / JAXA † JAXA ...
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DOI: 10.13009/EUCASS2019-284 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Guidance and Control Strategy for the CALLISTO Flight Experiment Marco Sagliano ...
152. Numerical Analysis of Aerodynamic Instability for HAYABUSA Type Reentry Capsule - Toru TSURUMOTO, Yusuke TAKAHASHI, Hiroshi TERASHIMA and Nobuyuki OSHIMA Hokkaido University, N13W8, Kita-ku, Sapporo, Hokkaido, ...
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DOI: 10.13009/EUCASS2019-288 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Numerical Analysis of Aerodynamic Instability for HAYABUSA Type Reentry Capsule Toru TSURUMOTO, Yusuke ...
153. Simulations of turbulence screens for ?ow and noise control in tandem cylinders - Wenqing Zhu , Zhixiang Xiao † , and Song Fu School of Aerospace Engineering, Tsinghua University Beijing, 100084, China ...
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DOI: 10.13009/EUCASS2019-289 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Simulations of turbulence screens for ?ow and noise control in tandem cylinders Wenqing ...
154. Advanced methodologies for conceptual design of commercial aircraft empennages - Eduardo González Hernando*, Fermín Navarro Medina**, J. Omar Martínez Lucci**, M. Ángel González Hernández*** *Future Projects ...
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DOI: 10.13009/EUCASS2019-290 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Advanced methodologies for conceptual design of commercial aircraft empennages Eduardo González Hernando*, ...
155. Anomalous Mesh Dependence of Adjoint Solutions Near Walls in Inviscid Flows Past Configurations with Sharp Trailing Edges - Carlos Lozano Computational Aerodynamics Group National Institute of Aerospace ...
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DOI: 10.13009/EUCASS2019-291 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Anomalous Mesh Dependence of Adjoint Solutions Near Walls in Inviscid Flows Past Configurations with Sharp ...
156. Cooling effect of gas injected through a non?symmetric slit of the wedge leading edge in a high speed flow - Pavel V. Chuvakhov*,**, Ivan V. Ezhov*,**, Andrey V. Novikov*,**, Eduard B. Vasilevsky* * Central ...
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DOI: 10.13009/EUCASS2019-293 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Cooling effect of gas injected through a non?symmetric slit of the wedge leading edge in a high speed flow Pavel ...
157. Multirow ?utter in low pressure turbines: Comparison of di?erent blade con?gurations - Oscar Bermejo , Juan Manuel Gallardo , Adrian Sotillo Ramos? and Carlos Augusto Diaz† Department of Simulation Technology ...
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DOI: 10.13009/EUCASS2019-295 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Multirow ?utter in low pressure turbines: Comparison of di?erent blade con?gurations Oscar ...
158. Experimental determination of thermodynamic properties of Hydrazine, MMH and NTO along the saturation line up to the critical point - Jouke Hijlkema and Marco de Rosa† ONERA / ESA† 31410, Mauzac, France ...
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DOI: 10.13009/EUCASS2019-297 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ??? Experimental determination of thermodynamic properties of Hydrazine, MMH and NTO along the ...
159. Numerical investigation of jet-wake interaction for a generic space launcher with a dual-bell nozzle - S. Loosen?† , M. Meinke?,?? and W. Schröder?,?? Institute of Aerodynamics and Chair of Fluid Mechanics ...
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DOI: 10.13009/EUCASS2019-300 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Numerical investigation of jet-wake interaction for a generic space launcher ...
160. Component tests of a LOX/methane full-expander cycle rocket engine: Single-shaft LOX/methane turbopump - Toru Tsukano*, Naoki Nagao*, Hiroshi Tomaru** and Toru Kuga** *JAXA 2-1-1, Sengen, Tsukuba-shi, ...
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DOI: 10.13009/EUCASS2019-301 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Component tests of a LOX/methane full-expander cycle rocket engine: Single-shaft LOX/methane turbopump Toru ...

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