Buoyancy and Stability
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Jean-Baptiste Charles Joseph Bélanger (1790-1874), the Backwater Equation and the Bélanger Equation
THE UNIVERSITY OF QUEENSLAND DIVISION OF CIVIL ENGINEERING REPORT CH69/08 JEAN-BAPTISTE CHARLES JOSEPH BÉLANGER (1790-1874), THE BACKWATER EQUATION AND THE BÉLANGER EQUATION AUTHOR: Hubert CHANSON HYDRAULIC MODEL REPORTS This report is published by the Division of Civil Engineering at the University of Queensland. Lists of recently-published titles of this series and of other publications are provided at the end of this report. Requests for copies of any of these documents should be addressed to the Civil Engineering Secretary. The interpretation and opinions expressed herein are solely those of the author(s). Considerable care has been taken to ensure accuracy of the material presented. Nevertheless, responsibility for the use of this material rests with the user. Division of Civil Engineering The University of Queensland Brisbane QLD 4072 AUSTRALIA Telephone: (61 7) 3365 3619 Fax: (61 7) 3365 4599 URL: http://www.eng.uq.edu.au/civil/ First published in 2008 by Division of Civil Engineering The University of Queensland, Brisbane QLD 4072, Australia © Chanson This book is copyright ISBN No. 9781864999211 The University of Queensland, St Lucia QLD JEAN-BAPTISTE CHARLES JOSEPH BÉLANGER (1790-1874), THE BACKWATER EQUATION AND THE BÉLANGER EQUATION by Hubert CHANSON Professor, Division of Civil Engineering, School of Engineering, The University of Queensland, Brisbane QLD 4072, Australia Ph.: (61 7) 3365 3619, Fax: (61 7) 3365 4599, Email: [email protected] Url: http://www.uq.edu.au/~e2hchans/ REPORT No. CH69/08 ISBN 9781864999211 Division of Civil Engineering, The University of Queensland August 2008 Jean-Baptiste BÉLANGER (1790-1874) (Courtesy of the Bibliothèque de l'Ecole Nationale Supérieure des Ponts et Chaussées) Abstract In an open channel, the transition from a high-velocity open channel flow to a fluvial motion is a flow singularity called a hydraulic jump. -
Principles of Instability and Stability in Digital PID Control Strategies and Analysis for a Continuous Alcoholic Fermentation Tank Process Start-Up
Preprints (www.preprints.org) | NOT PEER-REVIEWED | Posted: 29 July 2019 doi:10.20944/preprints201809.0332.v2 Principles of Instability and Stability in Digital PID Control Strategies and Analysis for a Continuous Alcoholic Fermentation Tank Process Start-up Alexandre C. B. B. Filhoa a Faculty of Chemical Engineering, Federal University of Uberlândia (UFU), Av. João Naves de Ávila 2121 Bloco 1K, Uberlândia, MG, Brazil. [email protected] Abstract The art work of this present paper is to show properly conditions and aspects to reach stability in the process control, as also to avoid instability, by using digital PID controllers, with the intention of help the industrial community. The discussed control strategy used to reach stability is to manipulate variables that are directly proportional to their controlled variables. To validate and to put the exposed principles into practice, it was done two simulations of a continuous fermentation tank process start-up with the yeast strain S. Cerevisiae NRRL-Y-132, in which the substrate feed stream contains different types of sugar derived from cane bagasse hydrolysate. These tests were carried out through the resolution of conservation laws, more specifically mass and energy balances, in which the fluid temperature and level inside the tank were the controlled variables. The results showed the facility in stabilize the system by following the exposed proceedings. Keywords: Digital PID; PID controller; Instability; Stability; Alcoholic fermentation; Process start-up. © 2019 by the author(s). Distributed under a Creative Commons CC BY license. Preprints (www.preprints.org) | NOT PEER-REVIEWED | Posted: 29 July 2019 doi:10.20944/preprints201809.0332.v2 1. -
Estimating Your Air Consumption
10/29/2019 Alert Diver | Estimating Your Air Consumption Estimating Your Air Consumption Advanced Diving Public Safety Diving By Mike Ange Mastering Neutral Buoyancy and Trim Military Diving Technical Diving Scientific Diving and Safety Program Oversight Seeing the Reef in a New Light ADVERTISEMENT Do you have enough breathing gas to complete the next dive? Here's how to find out. It is a warm clear day, and the Atlantic Ocean is like glass. As you drop into the water for a dive on North Carolina's famous U-352 wreck, you can see that the :: captain has hooked the wreck very near the stern. It is your plan to circumnavigate the entire structure and get that perfect photograph near the exposed bow torpedo tube. You descend to slightly below 100 feet, reach the structure and take off toward the bow. Unfortunately, you are only halfway, just approaching the conning tower, when your buddy signals that he is running low on air. Putting safety first, you return with him to the ascent line — cursing the lost opportunity and vowing to find a new buddy. If you've ever experienced the disappointment of ending a dive too soon for lack of breathing gas or, worse, had to make a hurried ascent because you ran out of air, it may surprise you to learn that your predicament was entirely predictable. With a little planning and some basic calculations, you can estimate how much breathing gas you will need to complete a dive and then take steps to ensure an adequate supply. It's a process that technical divers live by and one that can also be applied to basic open-water diving. -
8. Decompression Procedures Diver
TDI Standards and Procedures Part 2: TDI Diver Standards 8. Decompression Procedures Diver 8.1 Introduction This course examines the theory, methods and procedures of planned stage decompression diving. This program is designed as a stand-alone course or it may be taught in conjunction with TDI Advanced Nitrox, Advanced Wreck, or Full Cave Course. The objective of this course is to train divers how to plan and conduct a standard staged decompression dive not exceeding a maximum depth of 45 metres / 150 feet. The most common equipment requirements, equipment set-up and decompression techniques are presented. Students are permitted to utilize enriched air nitrox (EAN) mixes or oxygen for decompression provided the gas mix is within their current certification level. 8.2 Qualifications of Graduates Upon successful completion of this course, graduates may engage in decompression diving activities without direct supervision provided: 1. The diving activities approximate those of training 2. The areas of activities approximate those of training 3. Environmental conditions approximate those of training Upon successful completion of this course, graduates are qualified to enroll in: 1. TDI Advanced Nitrox Course 2. TDI Extended Range Course 3. TDI Advanced Wreck Course 4. TDI Trimix Course 8.3 Who May Teach Any active TDI Decompression Procedures Instructor may teach this course Version 0221 67 TDI Standards and Procedures Part 2: TDI Diver Standards 8.4 Student to Instructor Ratio Academic 1. Unlimited, so long as adequate facility, supplies and time are provided to ensure comprehensive and complete training of subject matter Confined Water (swimming pool-like conditions) 1. -
Control Theory
Control theory S. Simrock DESY, Hamburg, Germany Abstract In engineering and mathematics, control theory deals with the behaviour of dynamical systems. The desired output of a system is called the reference. When one or more output variables of a system need to follow a certain ref- erence over time, a controller manipulates the inputs to a system to obtain the desired effect on the output of the system. Rapid advances in digital system technology have radically altered the control design options. It has become routinely practicable to design very complicated digital controllers and to carry out the extensive calculations required for their design. These advances in im- plementation and design capability can be obtained at low cost because of the widespread availability of inexpensive and powerful digital processing plat- forms and high-speed analog IO devices. 1 Introduction The emphasis of this tutorial on control theory is on the design of digital controls to achieve good dy- namic response and small errors while using signals that are sampled in time and quantized in amplitude. Both transform (classical control) and state-space (modern control) methods are described and applied to illustrative examples. The transform methods emphasized are the root-locus method of Evans and fre- quency response. The state-space methods developed are the technique of pole assignment augmented by an estimator (observer) and optimal quadratic-loss control. The optimal control problems use the steady-state constant gain solution. Other topics covered are system identification and non-linear control. System identification is a general term to describe mathematical tools and algorithms that build dynamical models from measured data. -
Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883
Journal of Aviation/Aerospace Education & Research Volume 13 Number 1 JAAER Fall 2003 Article 1 Fall 2003 Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883 Thomas Forenz Follow this and additional works at: https://commons.erau.edu/jaaer Scholarly Commons Citation Forenz, T. (2003). Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883. Journal of Aviation/Aerospace Education & Research, 13(1). https://doi.org/10.15394/ jaaer.2003.1559 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Forenz: Assessing the Evolution of the Airborne Generation of Thermal Lif Thermal Lift ASSESSING THE EVOLUTION OF THE AIRBORNE GENERATION OF THERMAL LIFT IN AEROSTATS 1783 TO 1883 Thomas Forenz ABSTRACT Lift has been generated thermally in aerostats for 219 years making this the most enduring form of lift generation in lighter-than-air aviation. In the United States over 3000 thermally lifted aerostats, commonly referred to as hot air balloons, were built and flown by an estimated 12,000 licensed balloon pilots in the last decade. The evolution of controlling fire in hot air balloons during the first century of ballooning is the subject of this article. The purpose of this assessment is to separate the development of thermally lifted aerostats from the general history of aerostatics which includes all gas balloons such as hydrogen and helium lifted balloons as well as thermally lifted balloons. -
Lecture 3 Buoyancy (Archimedes' Principle)
LECTURE 3 BUOYANCY (ARCHIMEDES’ PRINCIPLE) Lecture Instructor: Kazumi Tolich Lecture 3 2 ¨ Reading chapter 11-7 ¤ Archimedes’ principle and buoyancy Buoyancy and Archimedes’ principle 3 ¨ The force exerted by a fluid on a body wholly or partially submerged in it is called the buoyant force. ¨ Archimedes’ principle: A body wholly or partially submerged in a fluid is buoyed up by a force equal to the weight of the displaced fluid. Fb = wfluid = ρfluidgV V is the volume of the object in the fluid. Demo: 1 4 ¨ Archimedes’ principle ¤ The buoyant force is equal to the weight of the water displaced. Lifting a rock under water 5 ¨ Why is it easier to lift a rock under water? ¨ The buoyant force is acting upward. ¨ Since the density of water is much greater than that of air, the buoyant force is much greater under the water compared to in the air. Fb air = ρair gV Fb water = ρwater gV The crown and the nugget 6 Archimedes (287-212 BC) had been given the task of determining whether a crown made for King Hieron II was pure gold. In the above diagram, crown and nugget balance in air, but not in water because the crown has a lower density. Clicker question: 1 & 2 7 Demo: 2 8 ¨ Helium balloon in helium ¨ Helium balloon in liquid nitrogen ¤ Demonstration of buoyancy and Archimedes’ principle Floatation 9 ¨ When an object floats, the buoyant force equals its weight. ¨ An object floats when it displaces an amount of fluid whose weight is equal to the weight of the object. -
Local and Global Instability of Buoyant Jets and Plumes
XXIV ICTAM, 21-26 August 2016, Montreal, Canada LOCAL AND GLOBAL INSTABILITY OF BUOYANT JETS AND PLUMES Patrick Huerre1a), R.V.K. Chakravarthy1 & Lutz Lesshafft 1 1Laboratoire d’Hydrodynamique (LadHyX), Ecole Polytechnique, Paris, France Summary The local and global linear stability of buoyant jets and plumes has been studied as a function of the Richardson number Ri and density ratio S in the low Mach number approximation. Only the m = 0 axisymmetric mode is shown to become globally unstable, provided that the local absolute instability is strong enough. The helical mode of azimuthal wavenumber m = 1 is always globally stable. A sensitivity analysis indicates that in buoyant jets (low Ri), shear is the dominant contributor to the growth rate, while, for plumes (large Ri), it is the buoyancy. A theoretical prediction of the Strouhal number of the self-sustained oscillations in helium jets is obtained that is in good agreement with experimental observations over seven decades of Richardson numbers. INTRODUCTION Buoyant jets and plumes occur in a wide variety of environmental and industrial contexts, for instance fires, accidental gas releases, ventilation flows, geothermal vents, and volcanic eruptions. Understanding the onset of instabilities leading to turbulence is a research challenge of great practical and fundamental interest. Somewhat surprisingly, there have been relatively few studies of the linear stability properties of buoyant jets and plumes, in contrast to the related purely momentum driven classical jet. In the present study, local and global stability analyses are conducted to account for the self-sustained oscillations experimentally observed in buoyant jets of helium and helium-air mixtures [1]. -
Buoyancy Compensator Owner's Manual
BUOYANCY COMPENSATOR OWNER’S MANUAL 2020 CE CERTIFICATION INFORMATION ECLIPSE / INFINITY / EVOLVE / EXPLORER BC SYSTEMS CE TYPE APPROVAL CONDUCTED BY: TÜV Rheinland LGA Products GmbH Tillystrasse 2 D-90431 Nürnberg Notified Body 0197 EN 1809:2014+A1:2016 CE CONTACT INFORMATION Halcyon Dive Systems 24587 NW 178th Place High Springs, FL 32643 USA AUTHORIZED REPRESENTATIVE IN EUROPEAN MARKET: Dive Distribution SAS 10 Av. du Fenouil 66600 Rivesaltes France, VAT FR40833868722 REEL Diving Kråketorpsgatan 10 431 53 Mölndal 2 HALCYON.NET HALCYON BUOYANCY COMPENSATOR OWNER’S MANUAL TRADEMARK NOTICE Halcyon® and BC Keel® are registered trademarks of Halcyon Manufacturing, Inc. Halcyon’s BC Keel and Trim Weight system are protected by U.S. Patents #5855454 and 6530725b1. The Halcyon Cinch is a patent-pending design protected by U.S. and European law. Halcyon trademarks and pending patents include Multifunction Compensator™, Cinch™, Pioneer™, Eclipse™, Explorer™, and Evolve™ wings, BC Storage Pak™, Active Control Ballast™, Diver’s Life Raft™, Surf Shuttle™, No-Lock Connector™, Helios™, Proteus™, and Apollo™ lighting systems, Scout Light™, Pathfinder™ reels, Defender™ spools, and the RB80™ rebreather. WARNINGS, CAUTIONS, AND NOTES Pay special attention to information provided in warnings, cautions, and notes accompanied by these icons: A WARNING indicates a procedure or situation that, if not avoided, could result in serious injury or death to the user. A CAUTION indicates any situation or technique that could cause damage to the product, and could subsequently result in injury to the user. WARNING This manual provides essential instructions for the proper fitting, adjustment, inspection, and care of your new Buoyancy Compensator. Because Halcyon’s BCs utilize patented technology, it is very important to take the time to read these instructions in order to understand and fully enjoy the features that are unique to your specific model. -
Future Towed Arrays - Operational Drivers and Technology Solutions
UDT 2019 Sensors & processing, Sonar arrays for improved operational capability Future towed arrays - operational drivers and technology solutions Prowse D. Atlas Elektronik UK. [email protected] Abstract — Towed array sonars provide a key capability in the suite of ASW sensors employed by undersea assets. The array lengths achievable and stand-off distance from platforms provide an advantage over other types of sonar in terms of the signal to noise ratio for detecting and classifying contacts of interest. This paper identifies the drivers for future towed arrays and explores technology solutions that could enable towed array sonar to provide the capability edge in the 21st Century. 1 Introduction 2.2 Maritime Autonomous Systems and sensors for ASW Towed arrays are a primary sensor for ASW acoustic detection and classification. They are used extensively by Recent advancement in autonomous systems and submarine and ASW surface combatants as part of their technology is opening up a plethora of new ASW armoury of tools against the submarine threat. As the capability opportunities and threats, including concepts nature of ASW evolves, the design and technology that involve the use of a towed array sensor on an incorporated into future ASW towed arrays will also need unmanned underwater or surface vessel in order to support to adapt. This paper examines the drivers behind the shift mission objectives. in ASW and explores the technology space that may provide leading edge for future capability. The use of towed arrays on autonomous systems has been studied to show how effective this type of capability can The scope of towed arrays that this paper considers be. -
Buoyancy Compensator Owner's Manual
BUOYANCY COMPENSATOR OWNER’S MANUAL BUOYANCY COMPENSATOR OWNER’S MANUAL Thank you for buying a DTD – DARE TO DIVE buoyancy compensator (BC). Our BC’s are manufactured from high quality materials. These materials are selected for their extreme durability and useful properties. Exceptional attention is paid to the technology and technical arrangement of all components during the manufacturing process. The advantages of DTD – DARE TO DIVE compensators are excellent craftsmanship, timeless design and variability; all thanks to production in the Czech Republic. TABLE OF CONTENTS CE certification information 2 Important warnings and precautions 2 Definitions 4 Overview of models 6 1. Wings 6 2. Backplates 7 Adjusting the backplate straps 8 1. Adjusting the shoulder straps and D-rings 8 2. Adjusting the crotch strap and D-rings 9 3. Adjusting the waist belt strap and D-ring 9 4. How to use the QUICK-FIX buckle 9 Threading the waist belt strap through the buckle 10 Tuning the compensator 11 1. Assembly of the compensator for using with single bottle 11 2. Assembly of the compensator for use with doubles 12 Optional equipment 13 1. Weighting systems 13 2. Buoy pocket 14 Pre-dive inspection of the compensator 14 Care, maintenance and storage recommendations 15 Service checks 15 General technical information 15 Operating temperature range 16 Warranty information 16 Manufacturer information 16 Annex 1 - detailed description of the wing label 17 Revised – February 2020 1 CE CERTIFICATION INFORMATION All DTD – DARE TO DIVE buoyancy compensators have been CE certified according to European standards. The CE mark governs the conditions for bringing Personal Protective Equipment to market and the health and safety requirements for this equipment. -
Astrophysical Fluid Dynamics: II. Magnetohydrodynamics
Winter School on Computational Astrophysics, Shanghai, 2018/01/30 Astrophysical Fluid Dynamics: II. Magnetohydrodynamics Xuening Bai (白雪宁) Institute for Advanced Study (IASTU) & Tsinghua Center for Astrophysics (THCA) source: J. Stone Outline n Astrophysical fluids as plasmas n The MHD formulation n Conservation laws and physical interpretation n Generalized Ohm’s law, and limitations of MHD n MHD waves n MHD shocks and discontinuities n MHD instabilities (examples) 2 Outline n Astrophysical fluids as plasmas n The MHD formulation n Conservation laws and physical interpretation n Generalized Ohm’s law, and limitations of MHD n MHD waves n MHD shocks and discontinuities n MHD instabilities (examples) 3 What is a plasma? Plasma is a state of matter comprising of fully/partially ionized gas. Lightening The restless Sun Crab nebula A plasma is generally quasi-neutral and exhibits collective behavior. Net charge density averages particles interact with each other to zero on relevant scales at long-range through electro- (i.e., Debye length). magnetic fields (plasma waves). 4 Why plasma astrophysics? n More than 99.9% of observable matter in the universe is plasma. n Magnetic fields play vital roles in many astrophysical processes. n Plasma astrophysics allows the study of plasma phenomena at extreme regions of parameter space that are in general inaccessible in the laboratory. 5 Heliophysics and space weather l Solar physics (including flares, coronal mass ejection) l Interaction between the solar wind and Earth’s magnetosphere l Heliospheric