- 261. IEMN/LEMAC-LICS Magneto-mechanical micro-actuators and active flow control: review of the last 15 years results - Talbi Abdelkrim(1), Viard Romain (1), Ghouila-Houri C?cile(1), Garnier Eric (2), Gallas ...
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- DOI: 10.13009/EUCASS2019-460 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) IEMN/LEMAC-LICS Magneto-mechanical micro-actuators and active flow control: review of the last 15 years ...
- 262. Application of CFD to WIG-craft motion control system design - S. A. Brodsky, A. V. Nebylov and A. I. Panferov International Institute for Advanced Aerospace Technologies of State University of Aerospace ...
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- DOI: 10.13009/EUCASS2019-461 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Application of CFD to WIG-craft motion control system design S. A. Brodsky, A. V. Nebylov and A. I. Panferov ...
- 263. Combustion Instability for Hybrid Rocket Motors with a Diaphragm - Jungpyo Leea,*, Sunjae Rheeb, Jinkon Kimc, Heejang Moond, Olexiy Shynkarenkoe, Domenico Simonef, Takakazu Moritag a,e,f University of ...
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- DOI: 10.13009/EUCASS2019-462 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Combustion Instability for Hybrid Rocket Motors with a Diaphragm Jungpyo Leea,*, Sunjae Rheeb, Jinkon Kimc, ...
- 264. Thermal pressure high temperature gradient micro-sensor for aerodynamic measurements - Ghouila-Houri C?cile(1), Talbi Abdelkrim(1), Viard Romain(2), Gallas Quentin(3), Merlen Alain(1), Pernod Philippe
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- DOI: 10.13009/EUCASS2019-464 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Thermal pressure high temperature gradient micro-sensor for aerodynamic measurements Ghouila-Houri C?cile(1), ...
- 265. ACTiVE ? Experimental set up and ?rst results of cold gas measurements for linear aerospike nozzles with secondary ?uid injection for thrust vectoring - Sieder-Katzmann, Jan ? , Propst, Martin , Stark, ...
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- DOI: 10.13009/EUCASS2019-465 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE ACTiVE ? Experimental set up and ?rst results of cold gas measurements for ...
- 266. MEMS calorimetric transducers for flow separation detection and control - Ghouila-Houri C?cile(1), Talbi Abdelkrim(1), Viard Romain(2), Gallas Quentin(3), Garnier Eric (4), Merlen Alain(1), Pernod Philippe(1) ...
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- DOI: 10.13009/EUCASS2019-466 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) MEMS calorimetric transducers for flow separation detection and control Ghouila-Houri C?cile(1), Talbi ...
- 267. Impulsive Multi-Rendezvous Trajectory Design and Optimization - Lorenzo Federici , Alessandro Zavoli ? and Guido Colasurdo Department of Mechanical and Aerospace Engineering, Sapienza University of Rome ...
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- DOI: 10.13009/EUCASS2019-469 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Impulsive Multi-Rendezvous Trajectory Design and Optimization Lorenzo Federici ...
- 268. Experimental Investigation of Showerhead injectors on Performance of a 1-kN Paraffin-Fueled Hybrid Rocket Motor - Mohammed Bouziane*, Artur Elias de Morais Bertoldi**, Praskovia Milova***, Patrick Hendrick*** ...
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- DOI: 10.13009/EUCASS2019-473 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental Investigation of Showerhead injectors on Performance of a 1-kN Paraffin-Fueled Hybrid Rocket ...
- 269. Finding the Parameters of Surface Roughness in Rarefied Gas Flow Solving the Inverse Problem - Olga A. Aksenova* and Iskander A. Khalidov** *St.-Petersburg Naval Polytechnic University, Department of Mathematics, ...
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- DOI: 10.13009/EUCASS2019-476 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Finding the Parameters of Surface Roughness in Rarefied Gas Flow Solving the Inverse Problem Olga A. Aksenova* ...
- 270. Direct Numerical Simulation of heat transfer in SMSP regenerative combustion chamber - F. Spalletta (1): E-mail: francesco.spalletta@service.avio.com D. Liuzzi (1) : E-mail: daniele.liuzzi@avio.com M. ...
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- DOI: 10.13009/EUCASS2019-479 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Direct Numerical Simulation of heat transfer in SMSP regenerative combustion chamber F. Spalletta (1): ...
- 271. ReFEx launch with a sounding rocket ? a challenging mission on a reliable carrier - Rainer Kirchhartz*, Alexander Schmidt** , Marcus H?rschgen-Eggers* and Alexander Kallenbach*
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- DOI: 10.13009/EUCASS2019-480 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) ReFEx launch with a sounding rocket ? a challenging mission on a reliable carrier Rainer Kirchhartz*, Alexander ...
- 272. Tunable Diode Laser Absorption Tomography for characterization of chemical species in aeronautical flames - Vincent Corbas, Fr?d?ric Champagnat, Guy Le Besnerais, Ajmal Mohamed ONERA 6 Chemin de la Vauve ...
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- DOI: 10.13009/EUCASS2019-482 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Tunable Diode Laser Absorption Tomography for characterization of chemical species in aeronautical flames Vincent ...
- 273. Improving safety requirements of the launch complex by developing modified launch vehicle control algorithms at the initial flight part - Maksim Trifonov and Vladimir Bobronnikov Moscow Aviation Institute ...
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- DOI: 10.13009/EUCASS2019-483 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Improving safety requirements of the launch complex by developing modified launch vehicle control algorithms ...
- 274. Compressive response and failure of a micromechanical model for confined unidirectional fiber-reinforced composites - Antonio Settanni* and Brina Blinzler** and Alessandro Ceruti*** *University of Bologna ...
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- DOI: 10.13009/EUCASS2019-485 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Compressive response and failure of a micromechanical model for confined unidirectional fiber-reinforced ...
- 275. THEORETICAL PERFORMANCE ANALYSIS OF HYBRID ROCKET PROPELLANTS AIMING AT THE DESIGN OF A TEST BENCH AND A PROPULSIVE SYSTEM - Mariana Conti Tarifa* and Loreto Pizzuti** *Federal University of ABC S?o Bernardo ...
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- DOI: 10.13009/EUCASS2019-488 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) THEORETICAL PERFORMANCE ANALYSIS OF HYBRID ROCKET PROPELLANTS AIMING AT THE DESIGN OF A TEST BENCH AND ...
- 276. Modified-Polygon Method for Point-in-Polygon Problem - Mostafa El-Salamony* and Amr Guaily**,*** *College of Engineering, Peking University, Beijing, China. elsalamony.mostafa@pku.edu.cn **Faculty of Engineering, ...
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- DOI: 10.13009/EUCASS2019-490 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Modified-Polygon Method for Point-in-Polygon Problem Mostafa El-Salamony* and Amr Guaily**,*** *College ...
- 277. 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOI NUMBER HERE - Optimisation in Active Flow Separation Control in Low-Pressure Turbines
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- DOI: 10.13009/EUCASS2019-492 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOI NUMBER HERE Optimisation in Active Flow Separation Control in Low-Pressure Turbines Yinzhu ...
- 278. Cessna Citation X Static Cruise Improvement using Morphing Wing Application on its Horizontal Tail - Marine Segui, Vittorio Rogoli and Ruxandra Mihaela Botez ETS, Laboratory of Active Controls, Avionics ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-494 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Cessna Citation X Static Cruise Improvement using Morphing Wing Application on its Horizontal Tail Marine ...
- 279. STUDY OF THE SHIELDING PERFORMANCE OF WHIPPLE SHIELD ENHANCED BY IMPEDANCE-GRADED MATERIALS - Pinliang Zhang*, Zizheng Gong**, Dongbo Tian, Guangming Song, Qiang Wu, Yan Cao, Ming Li *Beijing Institute ...
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- DOI: 10.13009/EUCASS2019-495 STUDY OF THE SHIELDING PERFORMANCE OF WHIPPLE SHIELD ENHANCED BY IMPEDANCE-GRADED MATERIALS Pinliang Zhang*, Zizheng Gong**, Dongbo Tian, Guangming Song, Qiang Wu, Yan Cao, ...
- 280. Methodology to Identify a Mathematical Model for Predicting Cessna Citation X Cruise Performance in Cruise Regime using Flight Manual Data - Georges Ghazi, Ruxandra Mihaela Botez, and Marina Kossinga-Yalemba ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-496 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Methodology to Identify a Mathematical Model for Predicting Cessna Citation X Cruise Performance in Cruise ...