- 21. The aerodynamic interference characteristics of TSTO vehicle stage separation - Yuelong He, Haichuan Yu*, Lan Chen, Dun Li
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-54 The aerodynamic interference characteristics of TSTO vehicle stage separation Yuelong He, Haichuan Yu*, Lan Chen, Dun Li (China Academy of Aerospace Aerodynamics, Beijing, ...
- 22. Experiments and optimization design of light-weight multilayer TPS - Xu Tengfei* , Qu Qiang, Xin Jianqiang, Chen Jingmao, Dong Yongpeng China Academy of Launch Vehicle Technology, Beijing 100076, China ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-61 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experiments and optimization design of light-weight multilayer TPS Xu Tengfei* , Qu Qiang, Xin Jianqiang, ...
- 23. Concept Study of S4TD based on Reliability Based Design Optimization - Hirokazu SUZUKI * *Japan Aerospace Exploration Agency 6-13-1 Osawa, Mitaka, Tokyo, Japan 181-0015, suzuki.hirokazu@jaxa.jp
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-62 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Concept Study of S4TD based on Reliability Based Design Optimization Hirokazu SUZUKI * *Japan Aerospace ...
- 24. Influence of Oscillator Phase Noise in Frequency-Based Location Methods for Mobile Exploration Robots - Francisco J. García-de-Quirós 1,3 *, Giammarco Radice 2 † and José Antonio Carrasco 3 ‡ 1 University ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-63 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Influence of Oscillator Phase Noise in Frequency-Based Location Methods for Mobile Exploration Robots Francisco ...
- 25. A Landing Buffer System for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle - Wang Dongliang*, Cui Qifeng, Luohaijun, Li Ming Aerospace System Engineering Shanghai, Shanghai 201109, P.R.China ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-69 A Landing Buffer System for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle Wang Dongliang*, Cui Qifeng, Luohaijun, Li Ming Aerospace System Engineering Shanghai, ...
- 26. Research on the fatigue life testing for composite wings - Xiaolei Ba*, Han Liu, Xiaolin Li, Dazheng Shen, Rong Yang *Beijing Institute of Structure and Environment Engineering No.8 Fucheng Road, Haidian ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-72 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Research on the fatigue life testing for composite wings Xiaolei Ba*, Han Liu, Xiaolin Li, Dazheng Shen, ...
- 27. Analysis of the 3-dimensional draping and permeability characteristics of woven fabric and optimization of the technological process for the complex shape aerospace structures - Pyi Phyo Maung* and Malysheva ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-77 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Analysis of the 3-dimensional draping and permeability characteristics of woven fabric and optimization ...
- 28. Numerical Simulation of Pitch-Damping Dynamic Derivatives - Yuanhong Ma*, Meng Lv**, Cheng Su*** China Academy of Aerospace Aerodynamics No.17 Yungang Road, Fengtai, Beijing, China, 100074 *yuanhongma@163.com ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-78 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Numerical Simulation of Pitch-Damping Dynamic Derivatives Yuanhong Ma*, Meng Lv**, Cheng Su*** China Academy ...
- 29. Combustion Modeling in Solid Rocket Motor Plumes - Tobias Ecker † , Sebastian Karl and Klaus Hannemann German Aerospace Center (DLR) Institute of Aerodynamics and Flow Technology Bunsenstr. 10, Göttingen, ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-79 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Combustion Modeling in Solid Rocket Motor Plumes Tobias Ecker † , Sebastian ...
- 30. Planetary Exploration of Saturn moons Dione and Enceladus - Juan R. Sanmartín* and J. Peláez**
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-81 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Planetary Exploration of Saturn moons Dione and Enceladus Juan R. Sanmartín* and J. Peláez** * Real Academia ...
- 31. Numerical simulation of ice accretion and consequent power loss estimation in wind turbine blades - Serkan Özgen*, Ezgi Aky?ld?z**, Ay?e Meriç Berker*** and Ali Çakmak† *Professor Middle East Technical ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-83 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Numerical simulation of ice accretion and consequent power loss estimation in wind turbine blades Serkan ...
- 32. DIAMOND WINGS IN SUPERSONIC FLOW WITH SLIP F.A. Maksimov1,2, N.A. Ostapenko1, M.A. Zubin1 - Institute of Mechanics, Lomonosov Moscow State University, Moscow, ostap@imec.msu.ru
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-85 DIAMOND WINGS IN SUPERSONIC FLOW WITH SLIP F.A. Maksimov1,2, N.A. Ostapenko1, M.A. Zubin1 1 Institute of Mechanics, Lomonosov Moscow State University, Moscow, This email address is being protected from spambots. You need JavaScript enabled to view it. 2 Institute ...
- 33. Simulation of Inflation Driving Deployment of Rolled Elastic Thin Wall Boom with Velcro Constraints - Jian Gao , Ping Tang , Chao Xie*, Fujun Peng *, Hua Zhang
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-86 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Simulation of Inflation Driving Deployment of Rolled Elastic Thin Wall Boom with Velcro Constraints Jian ...
- 34. Numerical investigation of transpiration cooling in supersonic nozzles - Valentina König † and Siegfried Müller and Michael Rom Institut für Geometrie und Praktische Mathematik, RWTH Aachen University ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-91 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Numerical investigation of transpiration cooling in supersonic nozzles Valentina ...
- 35. Investigation on the supplementary combustion scheme for the divergent section of a solid rocket engine nozzle - Zhao-bo Du College of Aerospace Science and Engineering, National University of Defense ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-92 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Investigation on the supplementary combustion scheme for the divergent section of a solid rocket engine ...
- 36. Wake Measurements of a MAV with Morphing Geometry - R. Bardera Mora*, A. A. Rodríguez Sevillano**, A. García-Magariño*, E. Barroso Barderas* * Instituto Nacional de Técnica Aeroespacial (INTA). Carretera ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-93 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Wake Measurements of a MAV with Morphing Geometry R. Bardera Mora*, A. A. Rodríguez Sevillano**, A. García-Magariño*, ...
- 37. Differential Game Guidance Law on Evader in Bearing-only Information Applications - Guo Hao, Yu Zhuoyang, Wang Xun and Chen Xuan Science and Technology on Space Physics Laboratory Beijing, 100076, Chi
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-94 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Differential Game Guidance Law on Evader in Bearing-only Information Applications Guo Hao, Yu Zhuoyang, ...
- 38. Structural design and analysis of a composite wing with high aspect ratio - Yu-shan Meng College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan 410073, ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-95 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Structural design and analysis of a composite wing with high aspect ratio Yu-shan Meng College of Aerospace ...
- 39. Research on Unsteady Plasma Plume by DSMC/PIC Hybrid Algorithms - Jie Li, Yongyuan Su, Zhenglei Fan, Jiawei Ye National University of Defense Technology, College of Aerospace Science and Engineering, Changsha ...
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-96 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Research on Unsteady Plasma Plume by DSMC/PIC Hybrid Algorithms Jie Li, Yongyuan Su, Zhenglei Fan, Jiawei ...
- 40. Technology acceleration process for the THEMIS low cost and reusable prototype - Jerome VILA* and Jeremie HASSIN** *ArianeWorks / CNES jerome.vila@arianeworks.com **ArianeWorks / CNES jeremie.hassin@a
- / Doc Indexer /
- DOI: 10.13009/EUCASS2019-97 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Technology acceleration process for the THEMIS low cost and reusable prototype Jerome VILA* and Jeremie ...