Will CFD Ever Replace Wind Tunnels Forbuilding Wind Simulations?
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Applications of Systems Engineering to the Research, Design, And
Applications of Systems Engineering to the Research, Design, and Development of Wind Energy Systems K. Dykes and R. Meadows With contributions from: F. Felker, P. Graf, M. Hand, M. Lunacek, J. Michalakes, P. Moriarty, W. Musial, and P. Veers NREL is a national laboratory of the U.S. Department of Energy, Office of Energy Efficiency & Renewable Energy, operated by the Alliance for Sustainable Energy, LLC. Technical Report NREL/TP-5000-52616 December 2011 Contract No. DE -AC36-08GO28308 Applications of Systems Engineering to the Research, Design, and Development of Wind Energy Systems Authors: K. Dykes and R. Meadows With contributions from: F. Felker, P. Graf, M. Hand, M. Lunacek, J. Michalakes, P. Moriarty, W. Musial, and P. Veers Prepared under Task No. WE11.0341 NREL is a national laboratory of the U.S. Department of Energy, Office of Energy Efficiency & Renewable Energy, operated by the Alliance for Sustainable Energy, LLC. National Renewable Energy Laboratory Technical Report NREL/TP-5000-52616 1617 Cole Boulevard Golden, Colorado 80401 December 2011 303-275-3000 • www.nrel.gov Contract No. DE-AC36-08GO28308 NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States government or any agency thereof. -
Numerical Optimization and Wind-Tunnel Testing of Low
Numerical Optimization and WindTunnel Testing of Low ReynoldsNumber Airfoils y Th Lutz W Wurz and S Wagner University of Stuttgart D Stuttgart Germany Abstract A numerical optimization to ol has been applied to the design of low Reynolds number airfoils Re The aero dynamic mo del is based on the Eppler co de with ma jor extensions A new robust mo del for the calculation of short n transitional separation bubbles was implemented along with an e transition criterion and Drelas turbulent b oundarylayer pro cedure with a mo died shap efactor relation The metho d was coupled with a commercial hybrid optimizer and applied to p erform unconstrained high degree of freedom optimizations with ob jective to minimize the drag for a sp ecied lift range One resulting airfoil was tested in the Mo del WindTunnel MWT of the institute and compared to the classical RG airfoil In order to allow a realistic recalculation of exp eriments conducted in the MWT the limiting nfactor was evaluated for this facility A sp ecial airfoil featuring an extensive instability zone was designed for this purp ose The investigation was supplemented by detailed measurements of the turbulence level Toget more insight in design guidelines for very low Reynolds numb er airfoils the inuence of variations of the leadingedge geometry on the aero dynamic characteristics was studied exp erimentally at Re Intro duction For the Reynoldsnumber regime of aircraft wingsections Re sophisticated di rect and inverse metho ds for airfoil analysis and design are available -
Comparison of Wind Tunnel Airfoil Performance Data with Wind Turbine Blade Data
SERI/TP-254·3799 UC Category: 261 DE90000343 Comparison of Wind Tunnel Airfoil Performance Data with Wind Turbine Blade Data C. P. Butterfield G. N. Scott W. Musial July 1990 presented at the 25th lntersociety Energy Conversion Engineering Conference (sponsored by American Institute of Aeronautics and Astronautics) Reno, Nevada 12-17 August 1990 Prepared under Task No. WE011 001 Solar Energy Research Institute A Division of Midwest Research Institute 1617 Cole Boulevard Golden, Colorado 80401-3393 Prepared for the U.S. Department of Energy Contract No. DE-AC02-83CH1 0093 NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, com pleteness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily con stitute or imply its endorsement, recommendation, or favoring by the United States government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States government or any agency thereof. Printed in the United States of America Available from: National Technical Information Service U.S. Department of Commerce 5285 Port Royal Road Springfield, VA 22161 Price: Microfiche A01 Printed Copy A02 Codes are used for pricing all publications. -
Upwind Sail Aerodynamics : a RANS Numerical Investigation Validated with Wind Tunnel Pressure Measurements I.M Viola, Patrick Bot, M
Upwind sail aerodynamics : A RANS numerical investigation validated with wind tunnel pressure measurements I.M Viola, Patrick Bot, M. Riotte To cite this version: I.M Viola, Patrick Bot, M. Riotte. Upwind sail aerodynamics : A RANS numerical investigation validated with wind tunnel pressure measurements. International Journal of Heat and Fluid Flow, Elsevier, 2012, 39, pp.90-101. 10.1016/j.ijheatfluidflow.2012.10.004. hal-01071323 HAL Id: hal-01071323 https://hal.archives-ouvertes.fr/hal-01071323 Submitted on 8 Oct 2014 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. I.M. Viola, P. Bot, M. Riotte Upwind Sail Aerodynamics: a RANS numerical investigation validated with wind tunnel pressure measurements International Journal of Heat and Fluid Flow 39 (2013) 90–101 http://dx.doi.org/10.1016/j.ijheatfluidflow.2012.10.004 Keywords: sail aerodynamics, CFD, RANS, yacht, laminar separation bubble, viscous drag. Abstract The aerodynamics of a sailing yacht with different sail trims are presented, derived from simulations performed using Computational Fluid Dynamics. A Reynolds-averaged Navier- Stokes approach was used to model sixteen sail trims first tested in a wind tunnel, where the pressure distributions on the sails were measured. -
10. Supersonic Aerodynamics
Grumman Tribody Concept featured on the 1978 company calendar. The basis for this idea will be explained below. 10. Supersonic Aerodynamics 10.1 Introduction There have actually only been a few truly supersonic airplanes. This means airplanes that can cruise supersonically. Before the F-22, classic “supersonic” fighters used brute force (afterburners) and had extremely limited duration. As an example, consider the two defined supersonic missions for the F-14A: F-14A Supersonic Missions CAP (Combat Air Patrol) • 150 miles subsonic cruise to station • Loiter • Accel, M = 0.7 to 1.35, then dash 25 nm - 4 1/2 minutes and 50 nm total • Then, must head home, or to a tanker! DLI (Deck Launch Intercept) • Energy climb to 35K ft, M = 1.5 (4 minutes) • 6 minutes at M = 1.5 (out 125-130 nm) • 2 minutes Combat (slows down fast) After 12 minutes, must head home or to a tanker. In this chapter we will explain the key supersonic aerodynamics issues facing the configuration aerodynamicist. We will start by reviewing the most significant airplanes that had substantial sustained supersonic capability. We will then examine the key physical underpinnings of supersonic gas dynamics and their implications for configuration design. Examples are presented showing applications of modern CFD and the application of MDO. We will see that developing a practical supersonic airplane is extremely demanding and requires careful integration of the various contributing technologies. Finally we discuss contemporary efforts to develop new supersonic airplanes. 10.2 Supersonic “Cruise” Airplanes The supersonic capability described above is typical of most of the so-called supersonic fighters, and obviously the supersonic performance is limited. -
Response of a Two-Story Residential House Under Realistic Fluctuating Wind Loads
Western University Scholarship@Western Electronic Thesis and Dissertation Repository 9-14-2010 12:00 AM Response of a Two-Story Residential House Under Realistic Fluctuating Wind Loads Murray J. Morrison The University of Western Ontario Supervisor Gregory A. Kopp The University of Western Ontario Graduate Program in Civil and Environmental Engineering A thesis submitted in partial fulfillment of the equirr ements for the degree in Doctor of Philosophy © Murray J. Morrison 2010 Follow this and additional works at: https://ir.lib.uwo.ca/etd Part of the Civil Engineering Commons, and the Structural Engineering Commons Recommended Citation Morrison, Murray J., "Response of a Two-Story Residential House Under Realistic Fluctuating Wind Loads" (2010). Electronic Thesis and Dissertation Repository. 13. https://ir.lib.uwo.ca/etd/13 This Dissertation/Thesis is brought to you for free and open access by Scholarship@Western. It has been accepted for inclusion in Electronic Thesis and Dissertation Repository by an authorized administrator of Scholarship@Western. For more information, please contact [email protected]. Response of a Two-Story Residential House Under Realistic Fluctuating Wind Loads (Spine title: Realistic Wind Loads on the Roof of a Two-Story House) (Thesis Format: Monograph) by Murray J. Morrison Department of Civil and Environmental Engineering Faculty of Engineering A thesis submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy School of Graduate and Postdoctoral Studies The University of Western Ontario London, Ontario, Canada © Murray J. Morrison 2010 THE UNIVERSITY OF WESTERN ONTARIO SCHOOL OF GRADUATE AND POSTDOCTORAL STUDIES CERTIFICATE OF EXAMINATION Supervisor Examiners ______________________________ ______________________________ Dr. -
Guidelines for Converting Between Various Wind Averaging Periods in Tropical Cyclone Conditions
GUIDELINES FOR CONVERTING BETWEEN VARIOUS WIND AVERAGING PERIODS IN TROPICAL CYCLONE CONDITIONS For more information, please contact: World Meteorological Organization Communications and Public Affairs Office Tel.: +41 (0) 22 730 83 14 – Fax: +41 (0) 22 730 80 27 E-mail: [email protected] Tropical Cyclone Programme Weather and Disaster Risk Reduction Services Department Tel.: +41 (0) 22 730 84 53 – Fax: +41 (0) 22 730 81 28 E-mail: [email protected] 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int D-WDS_101692 WMO/TD-No. 1555 GUIDELINES FOR CONVERTING BETWEEN VARIOUS WIND AVERAGING PERIODS IN TROPICAL CYCLONE CONDITIONS by B. A. Harper1, J. D. Kepert2 and J. D. Ginger3 August 2010 1BE (Hons), PhD (James Cook), Systems Engineering Australia Pty Ltd, Brisbane, Australia. 2BSc (Hons) (Western Australia), MSc, PhD (Monash), Bureau of Meteorology, Centre for Australian Weather and Climate Research, Melbourne, Australia. 3BSc Eng (Peradeniya-Sri Lanka), MEngSc (Monash), PhD (Queensland), Cyclone Testing Station, James Cook University, Townsville, Australia. © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0) 22 730 84 03 P.O. Box 2300 Fax: +41 (0) 22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] NOTE The designations employed in WMO publications and the presentation of material in this publication do not imply the expression of any opinion whatsoever on the part of the Secretariat of WMO concerning the legal status of any country, territory, city or area or of its authorities, or concerning the delimitation of its frontiers or boundaries. -
Modulhandbuch Wind Engineering
Module Handbook - Master „Wind Engineering“ 1 Module Handbook Master “Wind Engineering” Last updated_August 2019 Module Handbook - Master „Wind Engineering“ 2 Table of content Table of content .................................................................................................................................. 2 Module overview ................................................................................................................................. 3 Electives ............................................................................................................................................... 4 Module number [1]: Scientific and Technical Writing......................................................................... 5 Module number [2]: Global Wind industry and environmental conditions........................................ 6 Module number [3]: Wind farm project management and GIS .......................................................... 8 Module number [4]: Advanced Engineering Mathematics ............................................................... 10 Module number [5]: Mechanical Engineering for Electrical Engineers ............................................. 11 Module number [6]: Electrical Engineering for Mechanical Engineers ............................................. 13 Module number [7]: German for foreign students ........................................................................... 14 Module number [8]: English for engineers ...................................................................................... -
01 Wind Tunnels
ExperimentalExperimental AerodynamicsAerodynamics Lecture 1: Introduction G. Dimitriadis Experimental Aerodynamics Introduction •! Experimental aerodynamics can have the following objectives: –!To measure the forces exerted by the air on moving bodies –!To measure the forces exerted by wind on static bodies –!To help develop or validate aerodynamic theories –!To help design moving or static bodies so as to optimize their aerodynamic efficiency Experimental Aerodynamics History (1) •! Aerodynamics means ‘air in motion’. The term was first documented in 1837. •! Humans have known that moving air can exert significant forces on bodies since the dawn of time. •! Aristotle (4th century BC) is recognized as the first to write that air has weight and that bodies moving through fluids are subjected to forces. Experimental Aerodynamics History (2) •! Archimedes (3rd century BC) formulated the theory of hydrostatic pressure •! Leonardo Da Vinci brought about two major advances in aerodynamics: –! He noticed that water in a river moves faster in places where the river is narrow (basics of Bernouli’s theorem) –! He also stated that the aerodynamic results are the same when a body moves through a fluid as when a fluid moves past a static body at the same velocity: The wind tunnel principle Experimental Aerodynamics Aerodynamic Experiments •! Experiments in aerodynamics (and fluid dynamics) can take many forms. •! Observations: –! Water speed in rivers (Da Vinci, 15th century) •! Measurements –! Drag proportional to object’s area (Da Vinci, 15th century) -
ESDU Catalogue 2020 Validated Engineering Design Methods ESDU Catalogue
ESDU Catalogue 2020 Validated Engineering Design Methods ESDU Catalogue About ESDU ESDU has over 70 years of experience providing engineers with the information, data, and techniques needed to continually improve fundamental design and analysis. ESDU provides validated engineering design data, methods, and software that form an important part of the design operation of companies large and small throughout the world. ESDU’s wide range of industry-standard design tools are presented in over 1500 design guides with supporting software. Guided and approved by independent international expert Committees, and endorsed by key professional institutions, ESDU methods are developed by industry for industry. ESDU’s staff of engineers develops this valuable tool for a variety of industries, academia, and government institutions. www.ihsesdu.com Copyright © 2020 IHS Markit. All Rights Reserved II ESDU Catalogue ESDU Engineering Methods and Software The ESDU Catalog summarizes more than 350 Sections of validated design and analysis data, methods and over 200 related computer programs. ESDU Series, Sections, and Data Items ESDU methods and information are categorized into Series, Sections, and Data Items. Data Items provide a complete solution to a specific engineering topic or problem, including supporting theory, references, worked examples, and predictive software (if applicable). Collectively, Data Items form the foundation of ESDU. Data Items are prepared through ESDU’s validation process which involves independent guidance from committees of international experts to ensure the integrity and information of the methods. Consequently, every Data Item is presented in a clear, concise, and unambiguous format, and undergoes periodic review to ensure accuracy. Sections are comprised of groups of Data Items. -
1912 - 2012 Centenary of the Eiffel Wind Tunnel "Le Vent, Mon Ennemi…" Gustave Eiffel
Scientific Technical Review, 2012,Vol.62,No.3-4,pp.3-13 3 UDK: 533.6.071.3:808.62-316 COSATI: 01-01 Gustave Eiffel and the Wind: A Pioneer in Experimental Aerodynamics Dijana Damljanović1) 1912 - 2012 Centenary of the Eiffel Wind Tunnel "Le vent, mon ennemi…" Gustave Eiffel GUSTAVE Eiffel (1832-1923) is a prominent name in the history of engineering and technology. Educated as a civil engineer at the École Centrale des Arts et Manufactures, Eiffel had a career spanned over fifty years during which he designed dozens of legendary iron and steel structures, including the Porto Viaduct in Portugal, the supporting structure for the Statue of Liberty in New York Harbor, and the Eiffel Tower in Paris – the structure that cemented his name in history. This long and successful career brought him considerable wealth, and late in his life he decided to invest in the newly emerging field of aeronautics. At the age when many people retire, Eiffel built and operated some of the finest aeronautical research tools of his day using his own funds. In 1909, at the foot of his famous tower, Gustave Eiffel built one of the first wind tunnels dedicated to a new science: Aerodynamics. In 1912, the wind tunnel was moved to Auteuil, in Paris, where it is still in operation. He gathered data systematically setting new standards for measurement accuracy. His wind tunnels and methods served as models for subsequent laboratories around the world. This article traces the evolution of Alexandre Gustave Eiffel as an engineer and scientist, and gives a short overview of the celebration of the centenary of the Eiffel wind tunnel at Auteuil. -
GRAY-THESIS-2017.Pdf
DESIGN AND DEVELOPMENT OF A CONTINUOUS, OPEN-RETURN TRANSONIC WIND TUNNEL FACILITY BY CODY GRAY THESIS Submitted in partial fulfillment of the requirements for the degree of Master of Science in Aerospace Engineering in the Graduate College of the University of Illinois at Urbana-Champaign, 2017 Urbana, Illinois Adviser: Assistant Professor Phillip J. Ansell Abstract A new transonic wind tunnel facility was designed and built on the University of Illinois at Urbana-Champaign campus to enhance testing capabilities of the transonic flow regime. The new tunnel will expand the experimental capabilities available to the Department of Aerospace Engineering at UIUC for studying and understanding topics such as compressible dynamic stall aerodynamics, shock buffet phenomenon and control, shock wave boundary layer ingestion to a propulsor, and other future research topics. The new wind tunnel is a rectangular testing facility with a 6 in (width) x 9 in (height) cross-sectional area in the test section. It is a continuous, open-return facility, capable of operating within a Mach number range of M=0-0.8, and possibly reaching M=0.85 or higher depending on the test section configuration. The wind tunnel was assembled and installed in the Aerodynamics Research Laboratory. The tunnel is driven by a centrifugal blower that exhausts the air back into the laboratory. The components designed for the tunnel were the nozzle, diffuser, test section, settling chamber, inlet flow conditioning section, and the structural assembly. The most significant challenges in the design and development of the tunnel were enveloped in the test section and suction plenum control system.