Modal Analysis of Pressures on a Full-Scale Spinnaker
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2020 Ecsa Phrf Regulations
2020 ECSA PHRF REGULATIONS These repairs and improvements have the potential to affect boat speed when compared to the base Performance Handicap Racing Fleet of the boat upon which the rating is established. It is the Eastern Connecticut Sailing Association same for newer boats that are modified. For this reason, modifications and significant repairs made to I. GENERAL REGULATIONS any boat need to be documented and evaluated, and ECSA Handicap ratings are determined for each boat rating adjustments considered on a case-by-case as the sum of its base boat rating and any basis to maintain fair racing for all. All restorations, adjustments applied that address modifications to repairs and modifications described below and listed the standard boat, its sail plan, spars, propulsion, in Section XI of these Regulations, whether etc. as outlined in this document. Base boat ratings performed by you, others or previous owners, must are established based on performance potential and be reported and noted on your PHRF application observation in accordance with the design of a whether or not they replicate the original design. standard boat, equipped as intended by the original Modifications of interest typically include changes to manufacturer with US Coast Guard required safety the hull shape or structure, appendages, spars or equipment, maintained in top racing condition and sail plan, boat weight or propulsion. While some sailed by competent crew. It is the aim of these modifications may be allowable under One-Design regulations to equitably assign handicaps, as Time class rules where all boats are the same, they may Correction Factors, for conditions likely to be found require a rating adjustment for racing under PHRF. -
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 -
Designing Sails Since 1969
SAILRITE SAIL KITS Designing sails since 1969. Catalina 30 Tall Rig Mainsail Kit by Frederick Leroy Carter F 31R Screecher Kit by Patrick Pettengill Capri 18 Main & Jib Sail Kits by Brent Stiles “ We built this sail ourselves!” Custom Lateen Main Kit by Steve Daigle -Karen Larson Building your own sail is a very rewarding and satisfying Each kit comes with the sail design data and a set of instructions experience. Not only is there a real sense of accomplishment, and illustrations that have been perfected from over 40 years of but the skills developed in the process will make you a more self- experience and feedback. Sail panels are pre-cut, labeled and reliant sailor. Sailrite makes the process very easy and affordable numbered for easy assembly. Panel overlap and hemming lines from start to finish by providing sail kits that include materials come plotted on each panel and double-sided tape is included used by professional sailmakers at up to 50% less the cost! to adhere panels together prior to sewing to ensure that draft and shape are maintained during construction. Batten pockets, Sailrite uses state-of-the-art design programs and hardware to windows, draft stripes, reef points, and other details will also prepare each kit. Sail panels and corner reinforcements are all come plotted on the appropriate panels if required for your sail. computer-cut and seaming lines are drawn along the edges. Draft, twist, and entry and exit curves are all carefully calculated, controlled, and positioned for each sail to maximize performance. Getting Started All materials are carefully selected by our sail designers to Getting started is easy and Sailrite’s expert staff is available toll best suit your application and only high quality sailcloths and free every working day to answer questions and help guide you laminates from Bainbridge, Challenge, Contender and others who through the ordering and construction process. -
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. -
The Sailing Magazine for the Rest of Us
The sailing magazine for the rest of us. 10 00 00 $8 (Canada $8 CDN) 10 0 62825 97035 7 goodoldboat.com Issue 128 September/October 2019 Automatic/Manual Inflatable PFD USCG Approved Type V with Type II Performance! Full 35 lbs buoyancy! Comfortable, low profile, with wide neoprene neckline. Universal sizing, fits 30"-65" chest. Hi-Vis inflation chamber. Durable 400 denier nylon. Super bright retro-reflective areas on front and a high-visibility BEACON logo on the back. H Reg 179.99 HAMILTON SAVE $ 99 $30 NEW! 149 ea Pre-order MARINE Part# Color Order# ™ HMI-BCNI35OG Orange/Gray 773536 today! HMI-BCNI35BG Blue/Light Gray 773535 BOATERS' STORE! Moisture Absorber Dries air in cabins, lockers, closets, rooms, basements and other enclosed State-of-the-art line areas. Super-dry concentrated pellet of premium coatings, formula absorbs up to 50% more adhesives and putties. moisture than flake formulas. Search# SYT- $ 29 7 ea MK-6912 Order# 144114 Hamilton Wayne Photo by Tea Tree Power® Mold & Mildew Eliminator Non-toxic, bio-degradable. Blended from 100% Australian tea tree oil. Available in gel or spray. Tarps Starting At • Lightweight Blue 3 GRADES, $ 99 • Premium White 27 SIZES! 17 ea • Super Heavy Duty Silver HAMILTON Search# FOR-77020 Search# STT- Premium 7 Mil. White Oil Absorbent Sheets Shrink Wrap Each 15" x 19" sheet CAN HELP! absorbs 13 to 25 times Some sizes are available its weight in oil, fuel Many Hamilton Marine employees maintain in clear and blue. Shrink and other hydrocar- their own boats. And there is no better teacher wrap accessories are also bons. -
Sailing Course Materials Overview
SAILING COURSE MATERIALS OVERVIEW INTRODUCTION The NCSC has an unusual ownership arrangement -- almost unique in the USA. You sail a boat jointly owned by all members of the club. The club thus has an interest in how you sail. We don't want you to crack up our boats. The club is also concerned about your safety. We have a good reputation as competent, safe sailors. We don't want you to spoil that record. Before we started this training course we had many incidents. Some examples: Ran aground in New Jersey. Stuck in the mud. Another grounding; broke the tiller. Two boats collided under the bridge. One demasted. Boats often stalled in foul current, and had to be towed in. Since we started the course the number of incidents has been significantly reduced. SAILING COURSE ARRANGEMENT This is only an elementary course in sailing. There is much to learn. We give you enough so that you can sail safely near New Castle. Sailing instruction is also provided during the sailing season on Saturdays and Sundays without appointment and in the week by appointment. This instruction is done by skippers who have agreed to be available at these times to instruct any unkeyed member who desires instruction. CHECK-OUT PROCEDURE When you "check-out" we give you a key to the sail house, and you are then free to sail at any time. No reservation is needed. But you must know how to sail before you get that key. We start with a written examination, open book, that you take at home. -
Further Devels'nent Ofthe Tunny
FURTHERDEVELS'NENT OF THETUNNY RIG E M H GIFFORDANO C PALNER Gi f ford and P art ners Carlton House Rlngwood Road Hoodl ands SouthamPton S04 2HT UK 360 1, lNTRODUCTION The idea of using a wing sail is not new, indeed the ancient junk rig is essentially a flat plate wing sail. The two essential characteristics are that the sail is stiffened so that ft does not flap in the wind and attached to the mast in an aerodynamically balanced way. These two features give several important advantages over so called 'soft sails' and have resulted in the junk rig being very successful on traditional craft. and modern short handed-cruising yachts. Unfortunately the standard junk rig is not every efficient in an aer odynamic sense, due to the presence of the mast beside the sai 1 and the flat shapewhich results from the numerousstiffening battens. The first of these problems can be overcomeby usi ng a double ski nned sail; effectively two junk sails, one on either side of the mast. This shields the mast from the airflow and improves efficiency, but it still leaves the problem of a flat sail. To obtain the maximumdrive from a sail it must be curved or cambered!, an effect which can produce over 5 more force than from a flat shape. Whilst the per'formanceadvantages of a cambered shape are obvious, the practical way of achieving it are far more elusive. One line of approach is to build the sail from ri gid componentswith articulated joints that allow the camberto be varied Ref 1!. -
East-1946.Pdf
YACHTING -THE u. s . ONE-DESIGN CLASS IDS ONE-DESIGN class, which is T sponsored by a group of yachtsmen The perm4nent b4ckst.,ywtll keep representing all three clubs at Marble head, bids fair to become one of our popu the rig in the bo"t while the run lar racmg classes. Developed on the boards ning b4ckst4y will be needed in p~liminary plans by Carl Alberg, of only to 4Ssure the jib st4nding Marblehead, who is as80ciated with the well or to t4ke the tug of the ~den office, the general dimensions of the '\ rspinn4ker~ !' "" new boat arc: length over all, 37' 9"; \ length on the water line, 24'; beam, 7'; draft, 5' 4"; displacement is 6450 pounds. \ Her sail area is 378 8quarc feet, of which 262 square feet is in the mainsail and 116 \ square feet in the jib. In addition, there is \ a genoa with an area of. 200 square feet and a parachute spinnaker. \ An interesting feature of the new boat is a light weight, portable cabin top · \ which is made in two sections and may be \ carried in bad weather or for overnight I cruising. The cockpit, with the cabin top · removed, runs all the way forward to the . \ mast to facilitate light sail handling with Fastenings will_be made of bronze, the out the necessity of going on deck. The keel will be of lead and her hollow spars helmsman is 80 placed that he will get no will be spruce. Fittings and rigging will be interference from his crew, yet he will be by Merriman Brothers. -
Melges 15 Speed Guide Before Stepping the Mast
MELGES 15 SPEED GUIDE Updated August 19, 2020 Racing sailboats is much different from the other sporting events. Sailing requires tuning for different wind and water conditions. Many of these tuning adjustments are small, yet critical. We have outlined the following tuning information for the Melges 15. The measurements achieved have been tested through countless hours on the water in a variety of conditions. What is truly unique with this guide is that we have simplified the tuning process in order to make the process easy for Melges sailors. You will be able to achieve newfound speed in your Melges 15 after following these simple steps. Melges will continue to bring you the very best in sailing service and technology. Additional resources can be found in our how-to videos and articles available on Melges.com. Our objective is to allow you to set the pace in your racing class. Melges 15 Rigging Tutorial: https://youtu.be/BdogJjXHcm0 BEFORE STEPPING THE MAST 1. Clean and lubricate turnbuckles, make sure that the top and bottom threaded studs are even in the turnbuckle tube. Make sure that your turnbuckles are loose with a ½ inch of thread showing on each end of the turnbuckle. 2. Position mast so that base is next to the mast step on deck and top end is resting in the boom rest support or on the transom of your boat. You can step the mast alone or with a helper holding the base of the mast. 3. Check all pins, wires and fittings for wear. Plug in the side stays. -
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.