Improving the Downwind Sail Design Process by Means of a Novel FSI Approach
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12.9 Gennaker February 2013 Setting up and Sailing with the 12.9 Gennaker
12.9 Gennaker February 2013 Setting up and sailing with the 12.9 Gennaker The 12.9 Gennaker is a new bigger gennaker for the Weta. The standard gennaker is 8 sqm and the 12.9 gennaker is 12.9 sqm. The sail is designed for light to moderate breezes to help sailors racing in mixed fleets to get to a downwind mark faster. It is not intended to replace the standard 8.0 gennaker and will be sold as an extra. It is intended that one design racing fleets will stick with the 8.0 gennaker. It’s hard to say exactly what the performance difference in the sails is as it changes for different wind strengths. But with the 12.9 sqm gennaker you can sail on a generally lower (more downwind) heading than you can with the 8.0 sqm gennaker. The biggest changes are seen in a steady light breeze before you can get the boat planing. So to put it very roughly if you have two boats, one with the 8.0 and one with the 12.9 and you point both boats in a hot/tight reaching angle the 8.0 will be faster for most conditions. If you then point both boats at a low/broad reaching angle the 12.9 will be faster in most conditions. So on a windy day someone might sail further but faster with the 8.0 and get to the mark quicker than someone with the 12.9 sail who is sailing slower but less distance. For instance when Chris and I were testing, we did a day on a lake. -
CHAPTER TWO - Static Aeroelasticity – Unswept Wing Structural Loads and Performance 21 2.1 Background
Static aeroelasticity – structural loads and performance CHAPTER TWO - Static Aeroelasticity – Unswept wing structural loads and performance 21 2.1 Background ........................................................................................................................... 21 2.1.2 Scope and purpose ....................................................................................................................... 21 2.1.2 The structures enterprise and its relation to aeroelasticity ............................................................ 22 2.1.3 The evolution of aircraft wing structures-form follows function ................................................ 24 2.2 Analytical modeling............................................................................................................... 30 2.2.1 The typical section, the flying door and Rayleigh-Ritz idealizations ................................................ 31 2.2.2 – Functional diagrams and operators – modeling the aeroelastic feedback process ....................... 33 2.3 Matrix structural analysis – stiffness matrices and strain energy .......................................... 34 2.4 An example - Construction of a structural stiffness matrix – the shear center concept ........ 38 2.5 Subsonic aerodynamics - fundamentals ................................................................................ 40 2.5.1 Reference points – the center of pressure..................................................................................... 44 2.5.2 A different -
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. -
Sunfish Sailboat Rigging Instructions
Sunfish Sailboat Rigging Instructions Serb and equitable Bryn always vamp pragmatically and cop his archlute. Ripened Owen shuttling disorderly. Phil is enormously pubic after barbaric Dale hocks his cordwains rapturously. 2014 Sunfish Retail Price List Sunfish Sail 33500 Bag of 30 Sail Clips 2000 Halyard 4100 Daggerboard 24000. The tomb of Hull Speed How to card the Sailing Speed Limit. 3 Parts kit which includes Sail rings 2 Buruti hooks Baiky Shook Knots Mainshoat. SUNFISH & SAILING. Small traveller block and exerts less damage to be able to set pump jack poles is too big block near land or. A jibe can be dangerous in a fore-and-aft rigged boat then the sails are always completely filled by wind pool the maneuver. As nouns the difference between downhaul and cunningham is that downhaul is nautical any rope used to haul down to sail or spar while cunningham is nautical a downhaul located at horse tack with a sail used for tightening the luff. Aca saIl American Canoe Association. Post replys if not be rigged first to create a couple of these instructions before making the hole on the boom; illegal equipment or. They make mainsail handling safer by allowing you relief raise his lower a sail with. Rigging Manual Dinghy Sailing at sailboatscouk. Get rigged sunfish rigging instructions, rigs generally do not covered under very high wind conditions require a suggested to optimize sail tie off white cleat that. Sunfish Sailboat Rigging Diagram elevation hull and rigging. The sailboat rigspecs here are attached. 650 views Quick instructions for raising your Sunfish sail and female the. -
Introduction
CHAPTER 1 Introduction "For some years I have been afflicted with the belief that flight is possible to man." Wilbur Wright, May 13, 1900 1.1 ATMOSPHERIC FLIGHT MECHANICS Atmospheric flight mechanics is a broad heading that encompasses three major disciplines; namely, performance, flight dynamics, and aeroelasticity. In the past each of these subjects was treated independently of the others. However, because of the structural flexibility of modern airplanes, the interplay among the disciplines no longer can be ignored. For example, if the flight loads cause significant structural deformation of the aircraft, one can expect changes in the airplane's aerodynamic and stability characteristics that will influence its performance and dynamic behavior. Airplane performance deals with the determination of performance character- istics such as range, endurance, rate of climb, and takeoff and landing distance as well as flight path optimization. To evaluate these performance characteristics, one normally treats the airplane as a point mass acted on by gravity, lift, drag, and thrust. The accuracy of the performance calculations depends on how accurately the lift, drag, and thrust can be determined. Flight dynamics is concerned with the motion of an airplane due to internally or externally generated disturbances. We particularly are interested in the vehicle's stability and control capabilities. To describe adequately the rigid-body motion of an airplane one needs to consider the complete equations of motion with six degrees of freedom. Again, this will require accurate estimates of the aerodynamic forces and moments acting on the airplane. The final subject included under the heading of atmospheric flight mechanics is aeroelasticity. -
How Do Airplanes
AIAA AEROSPACE M ICRO-LESSON Easily digestible Aerospace Principles revealed for K-12 Students and Educators. These lessons will be sent on a bi-weekly basis and allow grade-level focused learning. - AIAA STEM K-12 Committee. How Do Airplanes Fly? Airplanes – from airliners to fighter jets and just about everything in between – are such a normal part of life in the 21st century that we take them for granted. Yet even today, over a century after the Wright Brothers’ first flights, many people don’t know the science of how airplanes fly. It’s simple, really – it’s all about managing airflow and using something called Bernoulli’s principle. GRADES K-2 Do you know what part of an airplane lets it fly? The answer is the wings. As air flows over the wings, it pulls the whole airplane upward. This may sound strange, but think of the way the sail on a sailboat catches the wind to move the boat forward. The way an airplane wing works is not so different. Airplane wings have a special shape which you can see by looking at it from the side; this shape is called an airfoil. The airfoil creates high-pressure air underneath the wing and low-pressure air above the wing; this is like blowing on the bottom of the wing and sucking upwards on the top of the wing at the same time. As long as there is air flowing over the wings, they produce lift which can hold the airplane up. You can have your students demonstrate this idea (called Bernoulli’s Principle) using nothing more than a sheet of paper and your mouth. -
Introduction to Aerospace Engineering
Introduction to Aerospace Engineering Lecture slides Challenge the future 1 Introduction to Aerospace Engineering Aerodynamics 11&12 Prof. H. Bijl ir. N. Timmer 11 & 12. Airfoils and finite wings Anderson 5.9 – end of chapter 5 excl. 5.19 Topics lecture 11 & 12 • Pressure distributions and lift • Finite wings • Swept wings 3 Pressure coefficient Typical example Definition of pressure coefficient : p − p -Cp = ∞ Cp q∞ upper side lower side -1.0 Stagnation point: p=p t … p t-p∞=q ∞ => C p=1 4 Example 5.6 • The pressure on a point on the wing of an airplane is 7.58x10 4 N/m2. The airplane is flying with a velocity of 70 m/s at conditions associated with standard altitude of 2000m. Calculate the pressure coefficient at this point on the wing 4 2 3 2000 m: p ∞=7.95.10 N/m ρ∞=1.0066 kg/m − = p p ∞ = − C p Cp 1.50 q∞ 5 Obtaining lift from pressure distribution leading edge θ V∞ trailing edge s p ds dy θ dx = ds cos θ 6 Obtaining lift from pressure distribution TE TE Normal force per meter span: = θ − θ N ∫ pl cos ds ∫ pu cos ds LE LE c c θ = = − with ds cos dx N ∫ pl dx ∫ pu dx 0 0 NN Write dimensionless force coefficient : C = = n 1 ρ 2 2 Vc∞ qc ∞ 1 1 p − p x 1 p − p x x = l ∞ − u ∞ C = ()C −C d Cn d d n ∫ pl pu ∫ q c ∫ q c 0 ∞ 0 ∞ 0 c 7 T=Lsin α - Dcosα N=Lcos α + Dsinα L R N α T D V α = angle of attack 8 Obtaining lift from normal force coefficient =α − α =α − α L Ncos T sin cl c ncos c t sin L N T =cosα − sin α qc∞ qc ∞ qc ∞ For small angle of attack α≤5o : cos α ≈ 1, sin α ≈ 0 1 1 C≈() CCdx − () l∫ pl p u c 0 9 Example 5.11 Consider an airfoil with chord length c and the running distance x measured along the chord. -
Activities on Dynamic Pressure
Activities on Dynamic Pressure Sari Saxholm Madrid and Tres Cantos, Spain 15 – 18 May 2017 Dynamic Measurements • Dynamic measurements are widely performed as a part of process control, manufacturing, product testing, research and development activities • Measurements of dynamic pressure have especially a key role in several demanding applications, e.g., in automotive, marine and turbine engines • However, if the sensors are calibrated with static techniques the sensor behavior and reliability of measurement results cannot be ensured in dynamically changing conditions • To guarantee the reliability of results there is the need of traceable methods for dynamic characterization of sensors 2 11th EURAMET General Assembly - 15 - 18 May 2017 EMRP IND09 Dynamic • This EMRP Project (Traceable dynamic measurement of mechanical quantities) was an unique opportunity to develop a new field of metrology • The aim was to develop devices and methods to provide traceability for dynamic measurements of the mechanical quantities force, torque, and pressure • Measurement standards were successfully developed for dynamic pressures for limited range Development work has continued after this EMRP Project: because the awareness of dynamic measurements, and challenges related with the traceability issues, has increased. 3 11th EURAMET General Assembly - 15 - 18 May 2017 Industry Needs • To cover, e.g., the motor industry measurement range better • To investigate the effects of pressure pulse frequency and shape • To investigate the effects of measuring media -
Furling Systems for Code 0 and Asymmetric Spinnakers
GX CX Furling systems for Code 0 and asymmetric spinnakers 3 best in apparent wind angles between 70° and 110°. and 70° between angles wind apparent in best sail is hoisted using the spinnaker halyard. This sail performs at its its at performs sail This halyard. spinnaker the using hoisted is sail 2 releasing the sheet and if possible bearing away. moderate and the the and moderate away. bearing possible if and sheet the releasing Prior to furling we recommend that power is taken out of the sail by by sail the of out taken is power that recommend we furling to Prior moderate winds and apparant wind angles between 70° and 110°. 110°. and 70° between angles wind apparant and winds moderate E G E L S • 0 S S 3 1 O - R 4 5 T A 5 5 B L 5 6 A S W N E E D sail which is cut flatter. Generally, the sail is developed for light and and light for developed is sail the Generally, flatter. cut is which sail G G G G G G G E E E G E E G E E G G E G G G E G E G E E E E E E E E E E G E E G G E G E E G E E E L G L G L L E E L E L E E G G E E G G E L E G E L E G E E E L G E L E L L G L E G L G E G E G L E G E G E E L E E E E E E E E G E L G E G E L E L E G E L G E E G E S E L S E S G E L E S L S S G E S L E L L E L E E S G E E E L E E L S E E L S S E S S S L E L E L L S L L E L S E E L E L S S S S L S L E L S S L L S S S S L S • • • S • • • L • S • • S S S S S S • • S • • • S • S • S S S S • • • S • S • • • S • • • • • • • • • • • • • • • • • • • • • • 0 0 • 0 0 0 0 0 S S S 0 S S S 0 S 0 0 0 0 S 0 S 0 S S 0 S S S S S 0 0 0 0 S 0 S 0 0 S S 0 0 S 0 0 0 S S -
A New Dynamic Pressure Source for the Calibration of Pressure Transducers
NBS Pubii - cations eferenc© sssfc in NBS TECHNICAL NOTE 914 *J *^AU Of U.S. DEPARTMENT OF COMMERCE/ National Bureau of Standards NATIONAL BUREAU OF STANDARDS 1 The National Bureau of Standards was established by an act of Congress March 3, 1901. The Bureau's overall goal is to strengthen and advance the Nation's science and technology and facilitate their effective application for public benefit. To this end, the Bureau conducts research and provides: (1) a basis for the Nation's physical measurement system, (2) scientific and technological services for industry and government, (3) a technical basis for equity in trade, and (4) technical services to promote public safety. The Bureau consists of the Institute for Basic Standards, the Institute for Materials Research, the Institute for Applied Technology, the Institute for Computer Sciences and Technology, and the Office for Information Programs. THE INSTITUTE FOR BASIC STANDARDS provides the central basis within the United States of a complete and consistent system of physical measurement; coordinates that system with measurement systems of other nations; and furnishes essential services leading to accurate and uniform physical measurements throughout the Nation's scientific community, industry, and commerce. The Institute consists of the Office of Measurement Services, the Office of Radiation Measurement and the following Center and divisions: Applied Mathematics — Electricity — Mechanics — Heat — Optical Physics — Center for Radiation Research: Nuclear Sciences; Applied Radiation — Laboratory Astrophysics 2 2 " 2 — Cryogenics — Electromagnetics — Time and Frequency . THE INSTITUTE FOR MATERIALS RESEARCH conducts materials research leading to improved methods of measurement, standards, and data on the properties of well-characterized materials needed by industry, commerce, educational institutions, and Government; provides advisory and research services to other Government agencies; and develops, produces, and distributes standard reference materials. -
2019 Boat Auction Catalog.Pub
SEND KIDS TO CAMP BOAT AUCTION & Nautical Fair Saturday, June 8 Nautical Yard Sale: 8:00 AM Registration:10:00 AM Auction:11:00 AM Where: Penobscot Bay YMCA Auctioneer: John Bottero YACHTS OF FUN FOR EVERYONE! • Live & Silent Auction • Dinghy Raffle • Food Concessions SPECIAL THANKS TO OUR EVENT SPONSORS LEARN MORE: 236.3375 ● WWW.PENBAYYMCA.ORG We are most grateful to everyone’s most generous support to help make our Boat Auction a success! JOHN BOTTERO THOMASTON PLACE AUCTION GALLERIES BOAT AUCTION COMMITTEE • Jim Bowditch • Paul Fiske • Larry Lehmann • Neale Sweet • Marty Taylor SEAWORTHY SPONSORS • Gambell & Hunter Sailmakers • Ocean Pursuits LLC • Maine Coast Construction • Wallace Events COMMUNITY PARTNERS • A Morning in Maine • Migis Lodge on Sebago Lake • Amtrak Downeaster • Once a Tree • Bay Chamber Concerts • Owls Head Transportation Museum • Bixby & Company • Portland Sea Dogs • Boynton-McKay Food Co. • Primo • Brooks, Inc. • Rankin’s Inc. • Camden Harbor Cruises • Red Barn Baking Company • Camden Snow Bowl • Saltwater Maritime • Cliff Side Tree • Samoset Resort • Down East Enterprise, Inc. • Schooner Appledore • Farnsworth Art Museum • Schooner Heritage • Flagship Cinemas • Schooner Olad & Cutter Owl • Golfer's Crossing • Schooner Surprise • Grasshopper Shop • Sea Dog Brewing Co. • Hampton Inn & Suites • Strand Theatre • House of Logan • The Inn at Ocean's Edge • Jacobson Glass Studio • The Study Hall • Leonard's • The Waterfront Restaurant • Maine Boats, Home and Harbors • UMaine Black Bears • Maine Wildlife Park • Whale's Tooth Pub • Maine Windjammer Cruises • Windjammer Angelique • Margo Moore Inc. • York's Wild Kingdom • Mid-Coast Recreation Center This is the Y's largest fundraising event of the year to help send kids to Summer Camp. -
Experimental Investigation of Asymmetric Spinnaker Aerodynamics Using Pressure and Sail Shape Measurements D
Experimental Investigation of Asymmetric Spinnaker Aerodynamics Using Pressure and Sail Shape Measurements D. Motta, R.G.J Flay, P.J Richards, D.J Le Pelley, Julien Deparday, Patrick Bot To cite this version: D. Motta, R.G.J Flay, P.J Richards, D.J Le Pelley, Julien Deparday, et al.. Experimental Investi- gation of Asymmetric Spinnaker Aerodynamics Using Pressure and Sail Shape Measurements. Ocean Engineering, Elsevier, 2014, a paraitre. 10.1016/j.oceaneng.2014.07.023. hal-01071557 HAL Id: hal-01071557 https://hal.archives-ouvertes.fr/hal-01071557 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. Science Arts & Métiers (SAM) is an open access repository that collects the work of Arts et Métiers ParisTech researchers and makes it freely available over the web where possible. This is an author-deposited version published in: http://sam.ensam.eu Handle ID: .http://hdl.handle.net/10985/8690 To cite this version : D MOTTA, R.G.J. FLAY, P.J. RICHARDS, D.J. LE PELLEY, Julien DEPARDAY, Patrick BOT - Experimental Investigation of Asymmetric Spinnaker Aerodynamics Using Pressure and Sail Shape Measurements - Ocean Engineering p.a paraitre - 2014 Any correspondence concerning this service should be sent to the repository Administrator : [email protected] Experimental Investigation of Asymmetric Spinnaker Aerodynamics Using Pressure and Sail Shape Measurements D.