FUTURE Flutter-Free Turbomachinery Blades
|
|
- Benedict Charles
- 5 years ago
- Views:
Transcription
1 Aero Days 2011, Madrid. FUTURE Flutter-Free Turbomachinery Blades Torsten Fransson, KTH Damian Vogt, KTH
2 A Typical Turbomachine RR Trent 1000 Picture courtesy of RR 2
3 What is it flutter? 3
4 Turbomachinery Flutter Flutter denotes a self-excited and self-sustained aeroelastic instability Very harmful unless properly damped Blades oscillate in traveling wave mode Neighbor blades usually lead to instability An isolated blade would not flutter 4
5 Why do turbomachinery blades flutter? 5
6 Underlying Mechanisms Flutter involves the interaction of fluid and structure Upon the motion of a component, the surrounding fluid will respond with an aerodynamic force The direction and phase of this force will lead to having the motion damped or augmented In case of augmentation, flutter will establish The character of the fluid response depends on many factors such as Geometrical aspects (i.e. profile shape, blade size, blade count) Operating point (idle, take-off, cruise) Ambient conditions (air temperature, etc) Dynamics (engine acceleration, deceleration) Flutter might establish only at very few of the above conditions. Due to its harmful character it must however be avoided at any cost 6
7 How can we ensure flutter-free turbomachinery blades? 7
8 Flutter-Free Turbomachinery Blades A good design does not flutter How to ensure a good design? Design for stability performing accurate predictions of the unsteady behavior of the structural dynamics (FEM) and aerodynamics (CFD) in a turbomachine Ensure large-enough stability limits (i.e. moderate changes in operating conditions, profile shape, etc will not directly lead to a flutter instability) A good design must also be economically viable Engine development costs and time Fulfilling other objectives such as performance, weight, manufacturing cost, maintainability etc During component design, industry nowadays largely relies on numerical simulations at affordable analysis costs (model size and run time) 8
9 How well are we to date doing on aeroelastic predictions? 9
10 Prediction Accuracy Test case: transonic compressor Each industry partner is using their own (trusted) aeroelastic analysis tool to analyze the aeroelastic behavior Variation of minimum aerodynamic damping with operating point π mass flow 10
11 Background Despite the high level of sophistication in today s numerical prediction tools, it is not uncommon that we have to deal with an accuracy of +-40% of predicted minimum aerodynamic damping In the present test case: 2 out of 5 predict flutter, 3 do not Test cases exist but these do not fully cover the spectrum needed for modern turbomachine designs Component types (blisks, bladed disks) Flow conditions (transonic flow, high loading, separations) Combinations of unsteady pressure and vibration data This empty spot shall be filled-in by the FUTURE project Establishing of new experimental test cases Extensive validation of state-of-the-art prediction tools 11
12 Presentation of FUTURE Project Flutter-Free Turbomachinery Blades 12
13 EU FP7 Project FUTURE Project aiming at the acquiring new sets of relevant validation data on turbomachinery aeroelasticity (compressor, turbine) and validating numerical tools Project coordinator: KTH, Prof Torsten Fransson Partners: 25 partners from industry, research institutes, academia Budget: 10.6M Duration: July 2008 June
14 FUTURE Project Partners Industry Research Institutes Academia 14
15 Project Concept Picture courtesy of RR Turbine Fan Compressor Aeroelastic experiments Aeroelastic computations Synthesis of experiments and computations x x x x x x 15
16 Project Structure Two main streaks of validation test cases as follows Transonic compressor High subsonic Low-Pressure Turbine (LPT) These test cases have been conceived within FUTURE Interconnected experiments Non-rotating cascade tests, controlled blade oscillation Rotating tests, multi-blade row, free and forced oscillation Mechanical characterizations of components (blisk, bladed disks) Application of novel measurement techniques such as PSP Interconnected computations Performed by virtually all partners in the project Pre-test predictions Post-test predictions 16
17 Work Package Structure WP1: Turbine and compressor cascade flutter Paolo Calza, Avio WP2: LPT Rotating rig flutter Roque Corral, ITP WP3: Multi-row compressor flutter Jan Östlund, Volvo Aero WP4: Synthesis of experiments and computations Detlef Korte, MTU WP5: Project management Damian Vogt, KTH Shortcut to Benefits 17
18 Presentation of FUTURE Test Cases 18
19 Transonic Compressor Design intent Aeroelastic stable operation at design point N rpm, φ ~ 0.6 Reduction of positive aerodynamic damping as stall line is approached 19
20 Compressor Flow Field 50% span 90% span ADP, Π
21 Compressor - Overview of Tests Non-rotating tests (isolated blade row, EPFL) Detailed steady aerodynamics Aerodynamic damping (controlled oscillation, free oscillation) Data: inlet/outlet flow parameters, blade loading, time-resolved blade surface pressure Rotating tests (1 ½ stage compressor, TUD) Detailed steady aerodynamics (blade loading, probe traverses) Mechanical characterization of rotor blisk (ECL) Damping measurements at various operating points Data: inlet/outlet flow parameters, blade loading, time-resolved blade surface pressure, blade vibration (tip-timing) 21
22 Non-Rotating Compressor Test Facility (EPFL) Annular cascade module 22
23 Rotating Compressor Test Facility (TUD) Rotor blisk 23
24 High Subsonic LPT Rotor Design intent Controlled aeroelastic instability at design point Limit Cycle Oscillations (LCO) N 2 416rpm, M 2 ~ 0.75 Goal: measurable LCO amplitudes displacement 24
25 LPT Rotor Flow Field SS PS Mach number 50% span Outlet ptot Surface oil flow 25
26 LPT - Overview of Tests Non-rotating tests (isolated blade row sector, KTH) Detailed steady aerodynamics Aerodynamic damping (controlled oscillation influence coefficients) Data: inlet/outlet flow parameters, blade loading, time-resolved blade surface pressure Rotating tests (1 stage LPT, CTA) Detailed steady aerodynamics (probe traverses) Two test objects: 1) cantilever 2) interlock Mechanical characterization of rotor bladed disks (AVIO) Damping measurements at various operating points Data: inlet/outlet flow parameters, blade vibration (tip-timing) 26
27 Non-Rotating LPT Test Facility (KTH) Annular sector cascade module 27
28 Cascade Flow Field Annular sector cascade 5 blades, 6 passages 70% span loading of rotating rig matched Fig with midspan loading Outlet Mach number distribution 28
29 Rotating LPT Test Facility (CTA) Cantilever configuration Interlock configuration Assembled rotor blades 29
30 What are the expected benefits of the FUTURE project? 30
31 Expected Benefits The FUTURE project shall contribute to making turbomachinery aeroelastic predictions more reliable Numerical tools validated on new, relevant and unique aeroelastic test cases that shall lead to best practice guidelines Achieving this will help making turbomachinery blades flutter-free make new aircraft engines more efficient cut development costs and time frames The FUTURE project will provide key enabling technologies towards a green, safe, reliable and affordable air transport of the future 31
32 Dissemination Great attention is given to the dissemination of project findings Feeding-back findings to education and life-long learning Examples Sharing of audiovisual instruction material from industry partners with universities Development of e-learning tools THRUST TurbomacHinery AeRomechanical UniverSity Training The world s first Masters programme in turbomachinery aeromechanics Upcoming THRUST+ Joint PhD programme on aeromechanics EXPLORE Aero World Virtual University 32
33 What do we envision after FUTURE? 33
34 Within the FUTURE project many questions will be answered but there might be unresolved topics at the end Having a strong project consortium and unique hardware in place, we envision research in the following directions Control of flutter (active, mistuning, novel damping concepts) Influence of flow distortion and impedance Flutter in the presence of other unsteady aerodynamic phenomena Development of new improved numerical models 34
35 35
Aeroelasticity of Turbomachines
MUSAF II Colloquium, Toulouse, France Aeroelasticity of Turbomachines Damian Vogt, formerly KTH (now University of Stuttgart) Torsten Fransson, KTH 2013-09-18 (Giles, 1991) 2 Content of Today s Talk Crash
More information432 JAXA Special Publication JAXA-SP E 5 pressure ratio % % 100% Fig. 1 Compressor map [2]: 1) surge line, 2) subsonic stalled
First International Symposium on Flutter and its Application, 2016 431 FLUTTER PREDICTION IN MODERN AIRCRAFT ENGINES AND GAS TURBINES Mikhail Kolotnikov +1, Pavel Makarov +2, Farrukh Abdukhakimov +3, and
More informationFlutter Testing. Wind Tunnel Testing (excerpts from Reference 1)
Flutter Testing In the early years of aviation, no formal flutter testing of aircraft was performed. Flutter was usually discovered by accident during flight of the aircraft. The pilot flew the aircraft
More informationSTALLING BEHAVIOUR OF A CONTRA-ROTATING AXIAL COMPRESSOR STAGE
STALLING BEHAVIOUR OF A CONTRA-ROTATING AXIAL COMPRESSOR STAGE by YASHPAL JAIN Thesis submitted in fulfilment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Mechanical Engineering
More informationCFD ANALYSIS TO INVESTIGATE THE EFFECT OF AXIAL SPACING IN A SINGLE STAGE TRANSONIC AXIAL FLOW COMPRESSOR
Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011) November 16-18, 2011, Bangalore, India CFD ANALYSIS TO INVESTIGATE THE EFFECT OF AXIAL SPACING IN A SINGLE STAGE TRANSONIC
More informationTHEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE
THEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE S.Ramamurthy 1, R.Rajendran 1, R. S. Dileep Kumar 2 1 Scientist, Propulsion Division, National Aerospace Laboratories, Bangalore-560017,ramamurthy_srm@yahoo.com
More informationWESEP 594 Research Seminar
WESEP 594 Research Seminar Aaron J Rosenberg Department of Aerospace Engineering Iowa State University Major: WESEP Co-major: Aerospace Engineering Motivation Increase Wind Energy Capture Betz limit: 59.3%
More informationInlet Influence on the Pressure and Temperature Distortion Entering the Compressor of an Air Vehicle
Distortion Entering the Compressor of an Air Vehicle P. Hendrick Université Libre de Bruxelles, ULB Avenue F.D. Roosevelt, 50 1050 Brussels BELGIUM patrick.hendrick@ulb.ac.be ABSTRACT One of the possible
More informationCasing wall static pressure distribution behavior in a centrifugal compressor with asymmetric inlet/outlet structures
Original Article Casing wall static pressure distribution behavior in a centrifugal compressor with asymmetric inlet/outlet structures Proc IMechE Part A: J Power and Energy 2019, Vol. 233(1 37 51! IMechE
More informationInvestigations on axial compressor cascades with aspiration on blades and hub
Investigations on axial compressor cascades with aspiration hub Thierry Obrecht Michel Dumas Elia Colombo - Cécile Deslot Snecma (Groupe Safran) Peter Ott Villaroche, France Laboratoire de Thermique Appliquée
More informationANALYSIS OF AERODYNAMIC CHARACTERISTICS OF A SUPERCRITICAL AIRFOIL FOR LOW SPEED AIRCRAFT
ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF A SUPERCRITICAL AIRFOIL FOR LOW SPEED AIRCRAFT P.Sethunathan 1, M.Niventhran 2, V.Siva 2, R.Sadhan Kumar 2 1 Asst.Professor, Department of Aeronautical Engineering,
More information1. Numerical simulation of AGARD WING 445.6
DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY Wei Qian*, Yuguang Bai*, Dong Wang** *School of Aeronautics and Astronautics, Faculty
More informationAn Impeller Blade Analysis of Centrifugal Gas Compressor Using CFD
An Impeller Blade Analysis of Centrifugal Gas Compressor Using CFD Vivek V. Kulkarni Department of Mechanical Engineering KLS Gogte Institute of Technology, Belagavi, Karnataka Dr. Anil T.R. Department
More informationCFD development for wind energy aerodynamics
CFD development for wind energy aerodynamics Hamid Rahimi, Bastian Dose, Bernhard Stoevesandt Fraunhofer IWES, Germany IEA Task 40 Kick-off Meeting 12.11.2017 Tokyo Agenda BEM vs. CFD for wind turbine
More informationWIND LOADS / MOORING & FISH TAILING. Arjen Koop, Senior Project Manager Offshore Rogier Eggers, Project Manager Ships
WIND LOADS / MOORING & FISH TAILING Arjen Koop, Senior Project Manager Offshore Rogier Eggers, Project Manager Ships OVERVIEW Wind Loads Wind shielding Fish tailing? 2 WIND LOADS FOR OFFSHORE MARS TLP
More informationFLOW CONSIDERATIONS IN INDUSTRIAL SILENCER DESIGN
FLOW CONSIDERATIONS IN INDUSTRIAL SILENCER DESIGN George Feng, Kinetics Noise Control, Inc., 3570 Nashua Drive, Mississauga, Ontario Vadim Akishin, Kinetics Noise Control, Inc., 3570 Nashua Drive, Mississauga,
More informationAxial and Centrifugal Compressor Mean Line Flow Analysis Method
7th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition - January 9, Orlando, Florida AIAA 9- Axial and Centrifugal Compressor Mean Line Flow Analysis Method Joseph
More informationThe EllipSys2D/3D code and its application within wind turbine aerodynamics
The EllipSys2D/3D code and its application within wind turbine aerodynamics Niels N. Sørensen Wind Energy Department, Risø DTU National Laboratory for Sustainable Energy and Dep. Civil Engineering, Aalborg
More informationLehigh-FIU Hybrid Wind Simulation Developments
Lehigh-FIU Hybrid Wind Simulation Developments 2018 NSF Lehigh-FIU NHERI Experimental Facilities User Workshop December 3 rd, 2018 Amal Elawady, PhD Assistant Professor Department of Civil and Environmental
More informationQuantification of the Effects of Turbulence in Wind on the Flutter Stability of Suspension Bridges
Quantification of the Effects of Turbulence in Wind on the Flutter Stability of Suspension Bridges T. Abbas 1 and G. Morgenthal 2 1 PhD candidate, Graduate College 1462, Department of Civil Engineering,
More informationOPTIMIZATION OF SINGLE STAGE AXIAL FLOW COMPRESSOR FOR DIFFERENT ROTATIONAL SPEED USING CFD
http:// OPTIMIZATION OF SINGLE STAGE AXIAL FLOW COMPRESSOR FOR DIFFERENT ROTATIONAL SPEED USING CFD Anand Kumar S malipatil 1, Anantharaja M.H 2 1,2 Department of Thermal Power Engineering, VTU-RO Gulbarga,
More informationNumerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential Groove Casing Treatment
Chinese Journal of Aeronautics 21(2008) 496-505 Chinese Journal of Aeronautics www.elsevier.com/locate/cja Numerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential
More informationV. A. Sedunin 1, O. V. Komarov 1, V. L. Blinov 1, A. V. Skorokhodov 1 & A. O. Procopets 2. Abstract. 1 Introduction
Energy Production and Management in the 21st Century, Vol. 1 707 The application of modern Computational Fluid Dynamics techniques for increasing the efficiency and stability of an axial compressor in
More informationAN ISOLATED SMALL WIND TURBINE EMULATOR
AN ISOLATED SMALL WIND TURBINE EMULATOR Md. Arifujjaman Graduate Student Seminar: Master of Engineering Faculty of Engineering and Applied Science Memorial University of Newfoundland St. John s, NL, Canada
More informationCourses of Instruction: Controlling and Monitoring of Pipelines
Courses of Instruction: Controlling and Monitoring of Pipelines Date December 2010 Dr. Peter Eschenbacher Partner Angergraben 4 85250 Altomünster Germany Tel. +49-(0)8254 / 99 69 57 Fax +49-(0)8254 / 99
More informationMeasurement and simulation of the flow field around a triangular lattice meteorological mast
Measurement and simulation of the flow field around a triangular lattice meteorological mast Matthew Stickland 1, Thomas Scanlon 1, Sylvie Fabre 1, Andrew Oldroyd 2 and Detlef Kindler 3 1. Department of
More informationA Research on the Airflow Efficiency Analysis according to the Variation of the Geometry Tolerance of the Sirocco Fan Cut-off for Air Purifier
A Research on the Airflow Efficiency Analysis according to the Variation of the Geometry Tolerance of the Sirocco Fan Cut-off for Air Purifier Jeon-gi Lee*, Choul-jun Choi*, Nam-su Kwak*, Su-sang Park*
More informationJ. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology.
J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology. < Helicopters Aircraft Gliders Sails > < Keels and rudders Hydrofoils
More informationNumerical Studies on the Effect of Slotted Casing Treatment on the Performance of a Transonic Axial Flow Compressor
Numerical Studies on the Effect of Slotted Casing Treatment on the Performance of a Transonic Axial Flow Compressor A. K. Shivayogi 1, Q. H. Nagpurwala 2 and M. D. Deshpande 3 1 - M. Sc. [Engg.] Student,
More informationSIMULATION OF ENVIRONMENTAL FLIGHT CONDITIONS
SIMULATION OF ENVIRONMENTAL FLIGHT CONDITIONS BY ADVANCED ALTITUDE SIMULATION Klaus SCHÄFER Institute of Space Propulsion, German Aerospace Centre (DLR) Lampoldshausen, 74239 Hardthausen, Germany klaus.schaefer@dlr.de
More informationIMPROVED BLADE PROFILES FOR HIGH LIFT LOW PRESSURE TURBINE APPLICATIONS
IMPROVED BLADE PROFILES FOR HIGH LIFT LOW PRESSURE TURBINE APPLICATIONS P. González *, I.Ulizar *, H.P.Hodson ** * ITP, Industria de Turbo Propulsores, SA. Parque Empresarial San Fernando Avda. Castilla
More informationUnsteady Shock Waves Vortex Shedding Entanglement in a Transonic Turbine Cascade
AFRL-AFOSR-UK-TR-2013-0033 Unsteady Shock Waves Vortex Shedding Entanglement in a Transonic Turbine Cascade Guillermo Paniagua Institut Von Karman DE Dynamique Des Fluides VZW Waterloosesteenweg 72 Sint-Genesius-Rode,
More informationPreventing unstable operation of a synthesis compressor using Dynamic System Simulation
Preventing unstable operation of a synthesis compressor using Dynamic System Simulation Mr. J.P.M. Smeulers, M.Sc.* TNO Science & Industry T: +31 15 269 2121 F: +31 15 269 2111 E: jan.smeulers@tno.nl *
More informationHigher Gas Turbine Operation Flexibility by Improved Diffuser Vanes of a Radial Compressor
Higher Gas Turbine Operation Flexibility by Improved Diffuser Vanes of a Radial Compressor STAR EUROPEAN CONFERENCE 2011 23 March 2011 Amsterdam, The Netherlands Dipl.-Ing. Anis Haj Ayed GmbH, Aachen,
More informationDesign and Analysis of a High Pressure Ratio Mixed Flow Compressor Stage
Design and Analysis of a High Pressure Ratio Mixed Flow Compressor Stage Gaurav Giri 1 and Abdul Nassar. 2 SoftInWay Turbomachinery Solutions Pvt Ltd. 70/10, Cunningham Road, Bangalore, KA, 560052, India
More informationCitation Journal of Thermal Science, 18(4),
NAOSITE: Nagasaki University's Ac Title Author(s) Noise characteristics of centrifuga diffuser (Noise reduction by means leading tip) Murakami, Tengen; Ishida, Masahiro; Citation Journal of Thermal Science,
More informationConventional Ship Testing
Conventional Ship Testing Experimental Methods in Marine Hydrodynamics Lecture in week 34 Chapter 6 in the lecture notes 1 Conventional Ship Testing - Topics: Resistance tests Propeller open water tests
More informationNávrh vratného kanálu u dvoustupňového kompresoru Return channel design of the two stage compressor
Návrh vratného kanálu u dvoustupňového kompresoru Return channel design of the two stage compressor J. Hrabovský, J. Vacula, M. Komárek L. K. Engineering, s.r.o C. Drápela, M. Vacek, J. Klíma PBS Turbo
More informationDynamic Analysis of a Multi-Stage Compressor Train. Augusto Garcia-Hernandez, Jeffrey A. Bennett, and Dr. Klaus Brun
Dynamic Analysis of a Multi-Stage Compressor Train Augusto Garcia-Hernandez, Jeffrey A. Bennett, and Dr. Klaus Brun Slide 2: Presenter/Author Bios Augusto Garcia-Hernandez Group Leader, Pipeline Simulation,
More informationThe Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration. M. Burak Şamşul
The Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration M. Burak Şamşul ITU AYOC 2014 - Milper Pervane Teknolojileri Company Profile MILPER is established in 2011 as a Research and Development
More informationNUMERICAL INVESTIGATION OF THE FLOW BEHAVIOUR IN A MODERN TRAFFIC TUNNEL IN CASE OF FIRE INCIDENT
- 277 - NUMERICAL INVESTIGATION OF THE FLOW BEHAVIOUR IN A MODERN TRAFFIC TUNNEL IN CASE OF FIRE INCIDENT Iseler J., Heiser W. EAS GmbH, Karlsruhe, Germany ABSTRACT A numerical study of the flow behaviour
More informationA COMPARATIVE STUDY OF MIX FLOW PUMP IMPELLER CFD ANALYSIS AND EXPERIMENTAL DATA OF SUBMERSIBLE PUMP
IMPACT: International Journal of Research in Engineering & Technology (IMPACT: IJRET) ISSN 2321-8843 Vol. 1, Issue 3, Aug 2013, 57-64 Impact Journals A COMPARATIVE STUDY OF MIX FLOW PUMP IMPELLER CFD ANALYSIS
More informationEffect of Inlet Clearance Gap on the Performance of an Industrial Centrifugal Blower with Parallel Wall Volute
International Journal of Fluid Machinery and Systems DOI: http://dx.doi.org/10.5293/ijfms.2013.6.3.113 Vol. 6, No. 3, July-September 2013 ISSN (Online): 1882-9554 Original Paper (Invited) Effect of Inlet
More informationInlet Influence on the Pressure and Temperature Distortion Entering the Compressor of an Air Vehicle
Distortion Entering the Compressor of an Air Vehicle P. Hendrick Université Libre de Bruxelles, ULB Avenue F.D. Roosevelt, 50 1050 Brussels BELGIUM patrick.hendrick@ulb.ac.be ABSTRACT One of the possible
More informationA NOVEL FLOATING OFFSHORE WIND TURBINE CONCEPT: NEW DEVELOPMENTS
A NOVEL FLOATING OFFSHORE WIND TURBINE CONCEPT: NEW DEVELOPMENTS L. Vita, U.S.Paulsen, T.F.Pedersen Risø-DTU Technical University of Denmark, Roskilde, Denmark luca.vita@risoe.dk Abstract: A novel concept
More informationEFFECT OF GEOMETRIC DISTORTION ON THE FLOW FIELD AND PERFORMANCE OF AN AXISYMMETRIC SUPERSONIC INTAKE
Indian J.Sci.Res.() : 909-99, 0 ISSN:50-08(Online) ISSN : 0976-876 (Print) EFFECT OF GEOMETRIC DISTORTION ON THE FLOW FIELD AND PERFORMANCE OF AN AXISYMMETRIC SUPERSONIC INTAKE MOHAMMAD FARAHANI a, ALIREZA
More informationAir-Sea Interaction Spar Buoy Systems
DISTRIBUTION STATEMENT A: Distribution approved for public release; distribution is unlimited Air-Sea Interaction Spar Buoy Systems Hans C. Graber CSTARS - University of Miami 11811 SW 168 th Street, Miami,
More informationWind effects on tall building frames-influence of dynamic parameters
Indian Journal of Science and Technology Vol. 3 No. 5 (May 21) ISSN: 974-6846 583 Wind effects on tall building frames-influence of dynamic parameters B. Dean Kumar 1 and B.L.P. Swami 2 1 Department of
More informationForest Winds in Complex Terrain
Forest Winds in Complex Terrain Ilda Albuquerque 1 Contents Project Description Motivation Forest Complex Terrain Forested Complex Terrain 2 Project Description WAUDIT (Wind Resource Assessment Audit and
More informationRedesign of Centrifugal PLACE FOR Compressor TITLE. Impeller by means of Scalloping
Redesign of Centrifugal PLACE FOR Compressor TITLE AUTHORS Impeller by means of Scalloping Kirill Grebinnyk, Aerodynamics Engineer, Sulzer (USA) Rob Widders, Engineering Manager, BOC (Australia) Kirill
More informationComputational fluid dynamics analysis of a mixed flow pump impeller
MultiCraft International Journal of Engineering, Science and Technology Vol. 2, No. 6, 2010, pp. 200-206 INTERNATIONAL JOURNAL OF ENGINEERING, SCIENCE AND TECHNOLOGY www.ijest-ng.com 2010 MultiCraft Limited.
More informationExperimental research on instability fault of high-speed aerostatic bearing-rotor system
Experimental research on instability fault of high-speed aerostatic bearing-rotor system Dongjiang Han 1, Changliang Tang 2, Jinfu Yang 3, Long Hao 4 Institute of Engineering Thermophysics, Chinese Academy
More informationCOMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES
5 th International Advanced Technologies Symposium (IATS 09), May 13-15, 2009, Karabuk, Turkey COMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES Emrah KULUNK a, * and Nadir YILMAZ b a, * New
More informationCFD SIMULATION STUDY OF AIR FLOW AROUND THE AIRFOIL USING THE MAGNUS EFFECT
Magnus effect, simulation, air flow Patryk SOKOŁOWSKI *, Jacek CZARNIGOWSKI **, Paweł MAGRYTA *** CFD SIMULATION STUDY OF AIR FLOW AROUND THE AIRFOIL USING THE MAGNUS EFFECT Abstract The article presents
More informationAmeliorating the Negative Damping in the Dynamic Responses of a Tension Leg Spar-Type Support Structure with a Downwind Turbine
1 Ameliorating the Negative Damping in the Dynamic Responses of a Tension Leg Spar-Type Support Structure with a Downwind Turbine Madjid Karimirad Torgeir Moan Author CeSOS Centre Centre for Ships for
More informationEXPERIMENTAL INVESTIGATION OF LIFT & DRAG PERFORMANCE OF NACA0012 WIND TURBINE AEROFOIL
EXPERIMENTAL INVESTIGATION OF LIFT & DRAG PERFORMANCE OF NACA0012 WIND TURBINE AEROFOIL Mr. Sandesh K. Rasal 1, Mr. Rohan R. Katwate 2 1 PG Student, 2 Assistant Professor, DYPSOEA Ambi Talegaon, Heat Power
More informationThe origin of gas pulsations in rotary PD compressors: ΔP or ΔU?
IOP Conference Series: Materials Science and Engineering PAPER OPEN ACCESS The origin of gas pulsations in rotary PD compressors: ΔP or ΔU? To cite this article: P X Huang et al 2015 IOP Conf. Ser.: Mater.
More informationJoint Industry Project (JIP) Shaft Dynamic Loads and Responses at Extreme Maneuvering and Ventilation of Mechanical Azimuthing Thrusters
Joint Industry Project (JIP) Shaft Dynamic Loads and Responses at Extreme Maneuvering and Ventilation of Mechanical Azimuthing Thrusters Page 1 Contents 1.0 Background... 3 2.0 SHARES JIP Objectives...
More informationDevelopment of TEU Type Mega Container Carrier
Development of 8 700 TEU Type Mega Container Carrier SAKAGUCHI Katsunori : P. E. Jp, Manager, Ship & Offshore Basic Design Department, IHI Marine United Inc. TOYODA Masanobu : P. E, Jp, Ship & Offshore
More informationThe Aerodynamic Design and Investigation of Loading Distribution of a Mixed Flow Compressor
Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 00 (2014) 000 000 www.elsevier.com/locate/procedia APISAT2014, 2014 Asia-Pacific International Symposium on Aerospace Technology,
More informationSTART UP MODELING OF KAIST MICRO MODULAR REACTOR COMPRESSOR USING BETA LINE METHOD WITH GAMMA+ CODE
The 6th International Supercritical CO2 Power Cycles Symposium March 27-29, 2018, Pittsburgh, Pennsylvania START UP MODELING OF KAIST MICRO MODULAR REACTOR COMPRESSOR USING BETA LINE METHOD WITH GAMMA+
More informationDetermination of Wind Turbine Blade Flapwise Bending Dynamics
Determination of Wind Turbine Blade Flapwise Bending Dynamics Chawin Chantharasenawong * and Warawut Tipkaew Department of Mechanical Engineering, King Mongkut s University of Technology Thonburi, Bangkok,
More informationExploration Series. AIRPLANE Interactive Physics Simulation Page 01
AIRPLANE ------- Interactive Physics Simulation ------- Page 01 What makes an airplane "stall"? An airplane changes its state of motion thanks to an imbalance in the four main forces acting on it: lift,
More informationNumerical simulations of a large offshore wind turbine exposed to turbulent inflow conditions
9 th European Seminar OWEMES 2017 Numerical simulations of a large offshore wind turbine exposed to turbulent inflow conditions Galih Bangga, Giorgia Guma, Thorsten Lutz and Ewald Krämer Institute of Aerodynamics
More informationVentilated marine propeller performance in regular and irregular waves; an experimental investigation
Ventilated marine propeller performance in regular and irregular waves; an experimental investigation G. K. Politis Department of Naval Architecture & Marine Engineering, National Technical University
More informationHigh fidelity gust simulations around a transonic airfoil
High fidelity gust simulations around a transonic airfoil AEROGUST Workshop 27 th - 28 th April 2017, University of Liverpool Presented by B. Tartinville (Numeca) Outline of the presentation 1Objectives
More informationGeometry Modification For Minimizing The Aeroelastics Effect
Geometry Modification For Minimizing The Aeroelastics Effect Fariduzzaman a, Subagyo a, Fadilah Hasim a and Matza Gusto Andika a a Aero-Gas dynamics and Vibration Laboratory (LAGG), BPPT, PUSPIPTEK, Serpong
More informationModeling of Scroll Compressor Using GT-Suite
Modeling of Scroll Compressor Using GT-Suite Ha-Duong Pham Sanden International (Europe) Ltd, German Branch hpham@sanden-europe.com Marek Lehocky Gamma Technologies GmbH M.Lehocky@gtisoft.com The copying,
More informationUnsteady airfoil experiments
Unsteady airfoil experiments M.F. Platzer & K.D. Jones AeroHydro Research & Technology Associates, Pebble Beach, CA, USA. Abstract This paper describes experiments that elucidate the dynamic stall phenomenon
More informationInjector Dynamics Assumptions and their Impact on Predicting Cavitation and Performance
Injector Dynamics Assumptions and their Impact on Predicting Cavitation and Performance Frank Husmeier, Cummins Fuel Systems Presented by Laz Foley, ANSYS Outline Overview Computational Domain and Boundary
More informationThe Estimation Of Compressor Performance Using A Theoretical Analysis Of The Gas Flow Through the Muffler Combined With Valve Motion
Purdue University Purdue e-pubs International Compressor Engineering Conference School of Mechanical Engineering The Estimation Of Compressor Performance Using A Theoretical Analysis Of The Gas Flow Through
More informationPROJECT and MASTER THESES 2016/2017
PROJECT and MASTER THESES 2016/2017 Below you ll find proposed topics for project and master theses. Most of the proposed topics are just sketches. The detailed topics will be made in discussion between
More informationStudy of Secondary Flow Modifications at Impeller Exit of a Centrifugal Compressor
Open Journal of Fluid Dynamics, 2012, 2, 248-256 http://dx.doi.org/10.4236/ojfd.2012.24a029 Published Online December 2012 (http://www.scirp.org/journal/ojfd) ABSTRACT Study of Secondary Flow Modifications
More informationPressure distribution of rotating small wind turbine blades with winglet using wind tunnel
Journal of Scientific SARAVANAN & Industrial et al: Research PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADES WITH WINGLET Vol. 71, June 01, pp. 45-49 45 Pressure distribution of rotating small wind
More informationDevelopment of a Simulation Model for Swimming with Diving Fins
Proceedings Development of a Simulation Model for Swimming with Diving Fins Motomu Nakashima 1, *, Yosuke Tanno 2, Takashi Fujimoto 3 and Yutaka Masutani 3 1 Department of Systems and Control Engineering,
More informationInternational Research Journal of Electronics and Computer Engineering Vol 1(3) Oct-Dec 2015
The PLC Based Design for the Air Compressor Control Process Miss Zahra Haghparas Electrical and electronic engineering Shiraz university of technology Shiraz, Iran f.haghparas@yahoo.com Ebrahim Abiri Associate
More informationAerodynamics of a wind turbine
Aerodynamics of a wind turbine Author: Kosmacheva Anna Supervisor: Jari Hämäläinen Lappeenranta University of Technology Technomatematics Introduction Wind turbine is a device that converts kinetic energy
More informationNumerical and Experimental Investigation of the Possibility of Forming the Wake Flow of Large Ships by Using the Vortex Generators
Second International Symposium on Marine Propulsors smp 11, Hamburg, Germany, June 2011 Numerical and Experimental Investigation of the Possibility of Forming the Wake Flow of Large Ships by Using the
More informationNumerical Analysis of the Tip Leakage Flow Field in a Transonic Axial Compressor with Circumferential Casing Treatment
Numerical Analysis of the Tip Leakage Flow Field in a Transonic Axial Compressor with Circumferential Casing Treatment G. Legras 1, N. Gourdain 2 and I. Trebinjac 1 1. LMFA Ecole Centrale de Lyon / Université
More informationAPPLICATION OF RESEARCH RESULTS AT LM WIND POWER
APPLICATION OF RESEARCH RESULTS AT LM WIND POWER Herning / March 27 / 2014 By Jesper Madsen Chief Engineer Aerodynamics and Acoustics AGENDA 1. EUDP Projects 1. DANAERO MW 2. Optimization of vortex generators
More informationWATER HYDRAULIC HIGH SPEED SOLENOID VALVE AND ITS APPLICATION
WATER HYDRAULIC HIGH SPEED SOLENOID VALVE AND ITS APPLICATION Akihito MITSUHATA *, Canghai LIU *, Ato KITAGAWA * and Masato KAWASHIMA ** * Department of Mechanical and Control Engineering, Graduate school
More informationProceedings of the ASME th Biennial Conference on Engineering Systems Design and Analysis ESDA2014 June 25-27, 2014, Copenhagen, Denmark
Proceedings of the ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis ESDA2014 June 25-27, 2014, Copenhagen, Denmark ESDA2014-20042 UNSTEADY FLOW SIMULATION IN SUCTION MUFFLER
More informationEvaluation of wind loads by a passive yaw control at the extreme wind speed condition and its verification by measurements
Evaluation of wind loads by a passive yaw control at the extreme wind speed condition and its verification by measurements Dec/11/2017 Soichiro Kiyoki Takeshi Ishihara Mitsuru Saeki Ikuo Tobinaga (Hitachi,
More informationApplied Fluid Mechanics
Applied Fluid Mechanics 1. The Nature of Fluid and the Study of Fluid Mechanics 2. Viscosity of Fluid 3. Pressure Measurement 4. Forces Due to Static Fluid 5. Buoyancy and Stability 6. Flow of Fluid and
More informationStability & Control Aspects of UCAV Configurations
Stability & Control Aspects of UCAV Configurations Paul Flux Senior Aerodynamicist BAE SYSTEMS Air Programmes Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection
More informationZIN Technologies PHi Engineering Support. PHi-RPT CFD Analysis of Large Bubble Mixing. June 26, 2006
ZIN Technologies PHi Engineering Support PHi-RPT-0002 CFD Analysis of Large Bubble Mixing Proprietary ZIN Technologies, Inc. For nearly five decades, ZIN Technologies has provided integrated products and
More informationOptimization of rotor profiles for energy efficiency by using chamber-based screw model
Optimization of rotor profiles for energy efficiency by using chamber-based screw model Dipl.-Ing. Sven Herlemann, Dr.-Ing. Jan Hauser, Dipl.-Ing. Norbert Henning, GHH RAND Schraubenkompressoren GmbH,
More informationOutside Air Nonresidential HVAC Stakeholder Meeting #2 California Statewide Utility Codes and Standards Program
1 Outside Air Nonresidential HVAC Stakeholder Meeting #2 California Statewide Utility Codes and Standards Program Jim Meacham, CTG Energetics Agenda 2 In Situ Testing Results Reduced Ventilation after
More informationEffects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor
Effects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor CONG-TRUONG DINH & KWANG-YONG KIM * Department of Mechanical Engineering Inha University 253 Yonghyun-Dong,
More informationJOURNAL PUBLICATIONS
1 JOURNAL PUBLICATIONS 71. Lee, T., Mageed, A., Siddiqui, B. and Ko, L.S., (2016) Impact of ground proximity on aerodynamic properties of an unsteady NACA 0012 airfoil, submitted to Journal of Aerospace
More information2-D Computational Analysis of a Vertical Axis Wind Turbine Airfoil
2-D Computational Analysis of a Vertical Axis Wind Turbine Airfoil Akshay Basavaraj1 Student, Department of Aerospace Engineering, Amrita School of Engineering, Coimbatore 641 112, India1 Abstract: This
More informationEXPERIMENTAL INVESTIGATIONS OF BARGE FLOATER WITH MOONPOOL FOR 5 MW WIND TURBINE
EXPERIMENTAL INVESTIGATIONS OF BARGE FLOATER WITH MOONPOOL FOR 5 MW WIND TURBINE 1 MR. G.VIJAYA KUMAR, 2 DR. R. PANNEER SELVAM 1 M.S. Research Scholar, Department of Ocean Engineering, IIT Madras, Chennai,
More informationA Characterization of Rotating Stall Behaviors in High and Low Speed Centrifugal Compressors
Purdue e-pubs International Compressor Engineering Conference School of Mechanical Engineering 1998 A Characterization of Rotating Stall Behaviors in High and Low Speed Centrifugal Compressors W. C. Oakes
More informationA numerical Euler-Lagrange method for bubble tower CO2 dissolution modeling
A numerical Euler-Lagrange method for bubble tower CO2 dissolution modeling Author: Daniel Legendre & Prof. Ron Zevenhoven Åbo Akademi University Thermal and Flow Engineering Laboratory Turku, Finland
More informationAerodynamic Analysis of Blended Winglet for Low Speed Aircraft
, July 1-3, 2015, London, U.K. Aerodynamic Analysis of Blended Winglet for Low Speed Aircraft Pooja Pragati, Sudarsan Baskar Abstract This paper provides a practical design of a new concept of massive
More informationAerodynamic study of a cyclist s moving legs using an innovative approach
Aerodynamic study of a cyclist s moving legs using an innovative approach Francesco Pozzetti 30 September 2017 Abstract During a period of four weeks in September, I completed a research project in fluid
More informationEFFECT OF GURNEY FLAPS AND WINGLETS ON THE PERFORMANCE OF THE HAWT
Chapter-6 EFFECT OF GURNEY FLAPS AND WINGLETS ON THE PERFORMANCE OF THE HAWT 6.1 Introduction The gurney flap (wicker bill) was a small flat tab projecting from the trailing edge of a wing. Typically it
More informationSubject: Structural Certification Criteria Date: 10/11/18 Policy No: PS-AIR for Antennas, Radomes, and Other External Modifications
Policy Statement Subject: Structural Certification Criteria Date: 10/11/18 Policy No: PS-AIR-25-17 for Antennas, Radomes, and Other External Modifications Initiated By: AIR-675 Summary This policy statement
More informationAN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS AN OSCILLATORY PITCHING NACA0012 AEROFOIL Ashim Yadav, Simon Prince & Jenny Holt School of Aerospace, Transport and Manufacturing,
More informationAIRFOIL PROFILE OPTIMIZATION OF AN AIR SUCTION EQUIPMENT WITH AN AIR DUCT
THERMAL SCIENCE, Year 2015, Vol. 19, No. 4, pp. 1217-1222 1217 AIRFOIL PROFILE OPTIMIZATION OF AN AIR SUCTION EQUIPMENT WITH AN AIR DUCT by Li QIU a,b, Rui WANG a,*, Xiao-Dong CHEN b, and De-Peng WANG
More information