1st International Conference. New Challenges In Aerospace Sciences -NCAS2013- November 7-8,2013 EDITURA PRINTECH BUCHAREST, ROMANIA

Transcription

1 1st International Conference New Challenges In Aerospace Sciences NCAS2013 November 7 8,2013 EDITURA PRINTECH BUCHAREST, ROMANIA

2 Delia Betak Mihai Vladimir Marija Ales NCAS 2013 TABLE OF CONTENTS INVITED PAPERS (KEY SPEAKERS) 1. Reducing Aviation Environmental Impact: The Key Role Of Research Networks Dominique Collin 2. Aviation and Environmental Management Dimitriu 3. Natural and Holistic Design of Thrust Propulsion System Pavel Virgil Stanciu, Cristina 4. Aerospace Engineering Education for Romanian and French Students Francois Grosjean SECTION 1: AERODYNAMICS AND AEROSPACE STRUCTURES 1. Quantitative Analysis of Aircraft Decompression Dalibor Rozehnal Horak, Petr Homola, 7 2. A Hybrid Aerodynamic Model for a Study of Pattern Helicopter Rotor Dynamics Ivan Dobrev, Fawaz Massouh, Michael Todorov RollDamping Measurement in the T38 Wind Tunnel Anastasijevic, Dragan Marinkovski, Jovan Isakovic Samardzic, Zoran Aerospace Engineering Education for Romanian and French students at ENSTA 19 Bretagne Francois Grosjean 5. Simulation of Reacting Flow Using Splitted Solver Vojtech Unsteady Measurements of Aerodynamic Characteristics of the Airfoil Dalibor Rozehnal Svoboda, Mixing of Neurotoxic Gases in HVAC Systems Nechifor, Paul Rosu, Valdenir Guimaraes MihailaAndres, Razvan Researches Concerninig Aircraft Wake Vortex Somoiag, loan Vedina, Pierre Ferrier CristianEmil Moldoveanu, Pamfil 34

3 AndreiFilip Valentin Constantin Test TeodorViorel Paul Daniel 9. About Smooth Particle Hydrodynamics (SPH) Method Used for Studying Impact 38 Cases Between Aerodynamic Surfaces and Foreign Bodies With Consistence of an Organic Tissue Mihai IvanicS, Vasile Nastasescu 10. Using of SPH Method for High Velocity Impact and Debris Cloud Numerical 43 Simulation Oana Mocian, Cristian Barbu, Vasile Nastasescu 11. Numerical Modeling and Simulation of the Air Blast and Its Effects on the Structures 48 Fiorina Bucur, Cristian Barbu 12. "J" Integral Applications. Crack Behaviour Comparitive Analysis in ElastoPlastic 54 and Liniary Elastic Modeled Mediums Daniela Barti, Anca Lupas, Roxana Nedelcu 13. The Shear StressStrain Curve Determination Using ators ional Split Hopkinson 58 Pressure Bar GigiIonuJ Nicolaescu, AmadoGeorge Stefan 14. Aspects Upon Nonconventional Methods Used Into Obtain MultiLayer Structures tefanmircea Mustafa, CiprianMarius Larco High Rate Delamination of Fibredux Composite Specimens Test Procedure Pahonie Radu Mode I High Rate Delamination of Fibredux Composite Specimens Pahonie Radu Results Light Weight Carbon Fiber CompressorImpeller/Blade Structural Design Olaru, Radu Mihalache, Valeriu Vilag, Dumitrita Gabor Nonlinear Buckling of Helicopter Tail Drive Shaft Due to Torsion Load Mihai Mihai laandres, Marian Vatavu Rosu, Stiffness Matrix Damage Analysis of a Composite Lamina Amado, Mustata Stefan Larco Ciprian, tefan Space Capsule Having Controled Flight Using Mouillard Effect Sandu, 86 Bogdan Sacuiu, Dumitru Amariutei, Iulian Viaduct, Razvan Carlanescu, Razvan Bimbasa 21. An Earth to Mars Mission Study Cojocaru, Mihai Valentin Predoi Improvement of Performances of Atm01 Aerial Target Eng. Dumitru Gustil Liviu Dragus, Ionu{ Ciobanu, Dynamic Flight and Control for Suborbital Launcher for Testing Chelaru, Cristian Barbu, Adrian Chelaru Control Synthesis Using Gradient Method for Suborbital Launcher Testing Part I Linearisation of the Movement Equations Pana, Adrian Chelaru Control Synthesis Using Gradient Method for Suborbital Launcher Testing control synthesis Part II Valentin Pana, Adrian Chelaru 107 2

4 Florin Mihalache Sequencing Marius Pamfil Vatavu Constantin Nechifor 26. Evaluation of Unguided Missile Trajectories Deviations Vedinas, CristianEmil Moldoveanu, Heloise Daude Somoiag, loan Study Concerning an Aerial Propeller Hub Under Nonlinear Static Loads RazvanGabriel, Dodu PetruEduart Aspects Regarding Aircraft Landing Gear Technical Requirements Marian In Flight Testing RaduCatalin Some Aspects of the Air Defense Missiles UpGrading Mihailescu, Malin Marinescu Radulescu, Cristina Study of Common Nose Cones With Ejctor Effect Used in Missiles Belega BogdanAlexandru Predictive Maintenance on Puma Helicopters PetruEduart DODU 138 SECTION 2: PROPULSION SYSTEMS 1. Combustion of Ecodiesel Kerosene Mixtures in Gasturbine Testing Rig Iva Ozana 142 Prah, Andreea Cristina Petcu, Razvan Carlanescu, Cornel Sandu, Milan Ermacora, Morana Jaganjac, Franz Tatzber, Neven Zarkovic 2. Measurement on Model of Internal Recirculation Channel of Centrifugal Compressor Martin Poledno, Petr Kmoch, Adolf Jilek On the Influence of the Centrifugal Compressor Rotor Blade Tip Clearance on the CFD 150 Simulation and the Optimization Bogdan G. Gherman, Valeriu Dragan 4. Experimental Measurements and Numerical Simulations in Bluff Body Flames Gabriel Florean, Bogdan George Gherman, Gheorghe Dumitrascu Stabilized New Constructive Solution for the Turbojet Combustion Chamber Paul Renard, Andra Negru Rotaru, Determining the Flue Gases Composition Rocket Turbopump Jeni A. Popescu, Valeriu A. Vilag at the Inlet of the Turbine Section for a Highlighting the Contribution af Aircraft Take Off Activity to Air Pollution from 166 Airport Areas by Nitrogen Oxides Monitoring Cretu Mihaiella, Teleaba Victoria, Deaconu Marius 8. Design of a Liquid Hydrogen Turbine to Drive a Rocket Engine Turbopump Cuciumita, Daniel Olaru, Jeni Popescu, Valeriu Vilag Cleopatra Propulsion Investigation in Aviation Accidents and Attribution Ing. Virgil Stanciu, Dr. Ing. Stefan Popescu, As. Ing. Casandra Balan Prof. Dr

5 Constantin Negrea RazvanViorel Prisacariu Sandu JenicaIleana Edu SECTION 3: A VIONICS 1.Co mputer Simulation in Use of Airplane Sharp Turn Maneuverability Predictions Martin Kmetik, Jaroslav Saiga Co mputerised Tester for Monitoring Inverters Dynamic Behaviour Corcau, Liviu Dinca, Teodor Lucian Grigorie A Closed Loop Capacitive Miniaturized Accelerometer Grigorie Teodor Lucian Petre, Edu loanaraluca, De termining The Aerodynamic Identification Coefficients of a SmallScale Paramotor Using a System 189 Technique RazvanViorel Mihai, Martin Timmerman,Aro n Neagu 5.Aut onomous Control of a SmallScale Paramotor Timmerman, Aran Neagu Mihai, Martin De velopment of the Error Model for a StrapDown Inertial Navigator George, Grigorie Teodor Lucian, Dodu Petru Eduart Dragos Exp ert System for Pilot Performance Assessment in Virtual Environment Gabriel Matei Pericle Ve rtical Component of Virtual Performances Flight and Physiological Profiling in Pilots' 210 Improving in Simulated Environment Pericle Gabriel Matei 9.Fabrica tion Technologies for Miniaturized Accelerometers and Raluca, Adochiei Gyros Felix, Negrea Petre, Radu Obreja, Costin Cepisca, Grigorie Teodor Lucian loana Applications of Gas Dynamic Functions in The Study of Fluid Flow Nozzles Through Laval 219 Nistor 11. Flying Wing With Electric Ducted Fan (EDF) Propulsion Boscoianu, Ionica CTrciu Vasile, Mircea Safety Management Systems And Aircraft Maintenance Organizations Zaharia, Florin Necula SorinEugen 228 4

6 Radu Comparison Anastasiei Petru Dan Martin Vlad Anca SECTION4: UAVSYSTEMS 1.EHAS Application to Existing Fighter Jet Weight Considerations Rozehnal, Slavomi'r Med Pelc, Dalibor GEOINT Applications for Critical Infrastructure Surveillance Raducanu, Paula 236 Mursa, Livia Ro u, Florentin Boda, Florin Georgescu, Radu Tanase, Laura Tartya 3.0n The Flight Stability of Quadcopters Gon9alvesCoelho Buse, Gabriela Ne tian, Antonio Modeli ng of The Real Movement in Resistant Environment of a Quadcopter Vasile Nufu 246 Between Wing Spar Torsion Panels and Wing Spar With Alternate "C" Profile 5.Num erical Simulation for Uav Wing Structure Mazare, Laura Jigleanu, Dan Stoica, Albert Plo nija Mazare, Camelia With EGNOS Extension to Eastern Europe: Flight Trials in Romania Radutu, Irina Stefanescu Olteanu, Alina The Accuracy of Digital Terrain Model from Lidar and Photogrammetric Data Paula, Boda Florentin, Raducanu Dan Th e Management of Human Activities in the Air Space Traian 263 AUTHORS INDEX 269 5