Principles of Environmental Physics Fourth Edition Principles of Environmental Physics Plants, Animals, and the Atmosphere Fourth Edition
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Gustave Eiffel, a Pioneer of Aerodynamics
Int. J. Engineering Systems Modelling and Simulation, Vol. 5, Nos. 1/2/3, 2013 3 Gustave Eiffel, a pioneer of aerodynamics Bruno Chanetz* Onera, 8 rue des Vertugadins, F-92 190 Meudon, France Fax: +33-1-46-23-51-58 and University Paris-Ouest, LTIE-GTE, EA 4415, 50 rue de Sèvres, F-92410 Ville d’Avray, France Fax: +33-1-40-97-48-73 E-mail: [email protected] E-mail: [email protected] *Corresponding author Martin Peter Laboratoire Aérodynamique Eiffel, 68 rue Boileau, F-75016 Paris E-mail: [email protected] Abstract: At the beginning of the 20th century, Gustave Eiffel contributes with Ludwig Prandtl to establish a new science: aerodynamics. He was going to study the forces to which he was confronted as engineer during his life: gravity and wind. Keywords: Eiffel wind tunnel; diffuser; laminar regime; turbulent regime; transition; drag of the sphere; Eiffel chamber. Reference to this paper should be made as follows: Chanetz, B. and Peter, M. (2013) ‘Gustave Eiffel, a pioneer of aerodynamics’, Int. J. Engineering Systems Modelling and Simulation, Vol. 5, Nos. 1/2/3, pp.3–7. Biographical notes: Bruno Chanetz joins Onera in 1983 as a Research Engineer. He was the Head of Hypersonic Group in 1990, Head of Hypersonic Hyperenthalpic Project in 1997 and Head of Experimental Simulation and Physics of Fluid Unit in 1998, then Deputy Director of the Fundamental and Experimental Aerodynamics Department in 2003. He was a Lecturer in Charge of the course ‘Boundary Layer’ at the Ecole Centrale de Paris from 1996 to 2003, then Associate Professor at the University of Versailles from 2003 to 2009. -
Brief History of the Early Development of Theoretical and Experimental Fluid Dynamics
Brief History of the Early Development of Theoretical and Experimental Fluid Dynamics John D. Anderson Jr. Aeronautics Division, National Air and Space Museum, Smithsonian Institution, Washington, DC, USA 1 INTRODUCTION 1 Introduction 1 2 Early Greek Science: Aristotle and Archimedes 2 As you read these words, there are millions of modern engi- neering devices in operation that depend in part, or in total, 3 DA Vinci’s Fluid Dynamics 2 on the understanding of fluid dynamics – airplanes in flight, 4 The Velocity-Squared Law 3 ships at sea, automobiles on the road, mechanical biomedi- 5 Newton and the Sine-Squared Law 5 cal devices, and so on. In the modern world, we sometimes take these devices for granted. However, it is important to 6 Daniel Bernoulli and the Pressure-Velocity pause for a moment and realize that each of these machines Concept 7 is a miracle in modern engineering fluid dynamics wherein 7 Henri Pitot and the Invention of the Pitot Tube 9 many diverse fundamental laws of nature are harnessed and 8 The High Noon of Eighteenth Century Fluid combined in a useful fashion so as to produce a safe, efficient, Dynamics – Leonhard Euler and the Governing and effective machine. Indeed, the sight of an airplane flying Equations of Inviscid Fluid Motion 10 overhead typifies the laws of aerodynamics in action, and it 9 Inclusion of Friction in Theoretical Fluid is easy to forget that just two centuries ago, these laws were Dynamics: the Works of Navier and Stokes 11 so mysterious, unknown or misunderstood as to preclude a flying machine from even lifting off the ground; let alone 10 Osborne Reynolds: Understanding Turbulent successfully flying through the air. -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
Pro.Ffress D &Dentsdc Raddo
Pro.ffress d_ &dentSdc Raddo FIFTEENTH GENERAL ASSEMBLY OF THE INTERNATIONAL SCIENTIFIC RADIO UNION September 5-15, 1966 Munich, Germany REPORT OF THE U.S.A. NATIONAL COMMITTEE OF THE INTERNATIONAL SCIENTIFIC RADIO UNION Publication 1468 NATIONAL ACADEMY OF SCIENCES NATIONAL RESEARCH COUNCIL Washington, D.C. 1966 Library of Congress Catalog Card No. 55-31605 Available from Printing and Publishing Office National Academy of Sciences 2101 Constitution Avenue Washington, D.C. 20418 Price: $10.00 October28,1966 Dear Dr. Seitz: I ampleasedto transmitherewitha full report to the NationalAcademy of Sciences--NationalResearchCouncil,onthe 15thGeneralAssemblyof URSIwhichwasheldin Munich,September5-15, 1966. TheUnitedStatesNationalCommitteeof URSIhasparticipatedin the affairs of the Unionfor forty-five years. It hashadmuchinfluenceonthe Unionas,.for example,in therecent creationof a Commissiononthe Mag- netosphere.ThisnewCommission,whichis nowvery strong,demonstrates the ability of theUnion,oneof ICSU'sthree oldest,to respondto the changingneedsof its field. AlthoughtheUnitedStatessendsthelargest delegationsof anycountry to the GeneralAssembliesof URSI,theyare neverthelessrelatively small becauseof thestrict mannerin whichURSIcontrolsthe size of its Assem- blies. This is donein order to preventineffectivenessthroughuncontrolled participationbyvery largenumbersof delegates.Accordingly,our delega- tions are carefully selected,andcomprisepeoplequalifiedto prepareand presentour NationalReportto the Assembly.Thepre-Assemblyreport is a report of progressin -
Mighty Eagle: the Development and Flight Testing of an Autonomous Robotic Lander Test Bed
Mighty Eagle: The Development and Flight Testing of an Autonomous Robotic Lander Test Bed Timothy G. McGee, David A. Artis, Timothy J. Cole, Douglas A. Eng, Cheryl L. B. Reed, Michael R. Hannan, D. Greg Chavers, Logan D. Kennedy, Joshua M. Moore, and Cynthia D. Stemple PL and the Marshall Space Flight Center have been work- ing together since 2005 to develop technologies and mission concepts for a new generation of small, versa- tile robotic landers to land on airless bodies, including the moon and asteroids, in our solar system. As part of this larger effort, APL and the Marshall Space Flight Center worked with the Von Braun Center for Science and Innovation to construct a prototype monopropellant-fueled robotic lander that has been given the name Mighty Eagle. This article provides an overview of the lander’s architecture; describes the guidance, navi- gation, and control system that was developed at APL; and summarizes the flight test program of this autonomous vehicle. INTRODUCTION/PROJECT BACKGROUND APL and the Marshall Space Flight Center (MSFC) technology risk-reduction efforts, illustrated in Fig. 1, have been working together since 2005 to develop have been performed to explore technologies to enable technologies and mission concepts for a new genera- low-cost missions. tion of small, autonomous robotic landers to land on As part of this larger effort, MSFC and APL also airless bodies, including the moon and asteroids, in our worked with the Von Braun Center for Science and solar system.1–9 This risk-reduction effort is part of the Innovation (VCSI) and several subcontractors to con- Robotic Lunar Lander Development Project (RLLDP) struct the Mighty Eagle, a prototype monopropellant- that is directed by NASA’s Planetary Science Division, fueled robotic lander. -
MDRS Final Summary Report – Crew 78 Vincent Beaudry, Kathryn Denning, Judah Epstein, Dirk Geeroms, Balwant Rai, Grier Wilt
MDRS final summary report – Crew 78 Vincent Beaudry, Kathryn Denning, Judah Epstein, Dirk Geeroms, Balwant Rai, Grier Wilt Introduction If interplanetary colonization is to be possible, humanity needs to learn as much as possible about how to rise to the challenges involved. One way to achieve this is, of course, through simulations. Our crew, the 78th in the Mars Desert Research Station simulation, was intensively international, composed of 2 Canadians (Kathryn Denning, Vincent Beaudry), 2 Americans (Judah Epstein, Grier Wilt), one Belgian (Dirk Geeroms) and one Indian (Balwant Rai). None of us had met before, and joining together to overcome language barriers and explore cultural differences provided us with an intense intercultural experience, surely akin to those which will be a part of future space exploration. As a group, we: developed our own knowledge of the challenges of space exploration; contributed to some ongoing MDRS research into extremophiles, environmental impact, and plant growth; furthered our individual projects in human physiology, long-distance teaching, and anthropology; acted as subjects for outside human factors researchers; and worked together to make life at the Hab go smoothly, including making some improvements to the Hab and to the EVA equipment. The Group Our crew was comprised of 6 individuals, with the following specialties: Vincent Beaudry was the commander, Judah Epstein the engineer and executive officer, Balwant Rai the scientist and health and security officer, Grier Wilt our biologist, Dirk Geeroms the teacher and astronomer, and Kathryn Denning our anthropologist and journalist. Although we all had our respective roles within this two weeks journey, we all enjoyed very much taking part in each others experiences and in the everyday tasks. -
Ancient Geodynamics and Global-Scale Hydrology on Mars
R EPORTS 15. ccs represents the CO2 concentration at the chloro- component and calculate eq from a weighting of plast surface, which is the limit of CA activity and is 75:25 C4 grasses:trees to allow for the presence of thus assumed to represent the site of CO2-H2Oin trees in savanna-type habitats. Group 9 (C3 grassland leaves. ccs is typically a midway value between those and agriculture) we assume comprises 25:50:25 for in the liquid-air interfaces and the sites of CO2 trees:C3 grasses:C4 grasses; the C3 and C4 grasses assimilation inside leaves (14). include some C3 herbs and C4 grass species as crops. 16. Supplementary data are available on Science Online 31. G. Hoffmann et al., in preparation. at www.sciencemag.org/cgi/content/full/291/5513/ 32. J. R. Ehleringer, T. E. Cerling, B. R. Helliker, Oecologia 2584/DC1. 112, 285 (1997). 17. M. D. Hatch, J. N. Burnell, Plant Physiol. 93, 825 33. G. J. Collatz, J. A. Berry, J. S. Clark, Oecologia 114, 441 (1990). (1998). 18. E. Utsoniyama, S. Muto, Physiol. Plant. 88, 413 34. J. Lloyd, G. D. Farquhar, Oecologia 99, 201 (1994). (1993). 35. M. Trolier, J. W. C. White, J. R. Lawrence, W. S. 19. A. Makino et al., Plant Physiol. 100, 1737 (1992) Broecker, J. Geophys. Res. 101, 25897 (1996). 20. G. A. Mills, H. C. Urey, J. Am. Chem. Soc. 62, 1019 36. R. A. Houghton, Tellus 51B, 298 (1999). (1940). 37. R. H. Waring, W. H. Schlesinger, Forest Ecosystems 21. J. S. -
O Lunar and Planetary Institute Provided by the NASA Astrophysics Data System RADAR ALTIMETRY of the LARGE ?.LARTIAN CRATERS
RADAR ALTIMETRY OF THE LARGE MARTIAN CRATERS, L. E. Roth, G. S. Downs, and R. S. Saunders, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91103; G. Schubert, Department of Earth and Space Sciences, University of California, Los Angeles, California 90024. The Goldstone Mars data (1,2) have been used to obtain detailed morpho- metric information on martian craters. Some qualitative results of this effort have been reported previously (3). Radar profiles of a total of 131 impact craters have been recognized. (The following symbols are used in the subsequent discussion: Ri (km) is crater depth and Dr (km) is rim-crest diameter (4)). The craters range in size from Dr " 20 km to Dr " 500 km, and are all located within a subequatorial belt of the cratered highlands, bounded by approximate latitudes of -14' and -21'. This belt constitutes about 8% of the total surface area of the planet. The current data coverage does not exceed approximately 25% of the area of the belt, i.e., about 2% of the area of the planet. Radar profiles of large craters with the visually flat floors show sub- dued crater rims (rarely higher than 300-400 meters), usually shallow interior walls, and little structural detail in the interior and the exterior walls. In contrast, the floors of the same craters often display topographic relief greater than the error in the range measurement. The largest craters (Dr > 125 km) show differing degrees of the floor level adjustment. The two extreme cases are the craters Bakhuysen (Dr = 140 km, (-23.0°, 344.0')) whose floor is almost 2500 m below the surrounding terrain, in sharp contrast with Denning (Dr = 140 km, (-17.8O, 326.5O)) whose floor is almost at the same level as the surrounding terrain. -
Outline of Physical Science
Outline of physical science “Physical Science” redirects here. It is not to be confused • Astronomy – study of celestial objects (such as stars, with Physics. galaxies, planets, moons, asteroids, comets and neb- ulae), the physics, chemistry, and evolution of such Physical science is a branch of natural science that stud- objects, and phenomena that originate outside the atmosphere of Earth, including supernovae explo- ies non-living systems, in contrast to life science. It in turn has many branches, each referred to as a “physical sions, gamma ray bursts, and cosmic microwave background radiation. science”, together called the “physical sciences”. How- ever, the term “physical” creates an unintended, some- • Branches of astronomy what arbitrary distinction, since many branches of physi- cal science also study biological phenomena and branches • Chemistry – studies the composition, structure, of chemistry such as organic chemistry. properties and change of matter.[8][9] In this realm, chemistry deals with such topics as the properties of individual atoms, the manner in which atoms form 1 What is physical science? chemical bonds in the formation of compounds, the interactions of substances through intermolecular forces to give matter its general properties, and the Physical science can be described as all of the following: interactions between substances through chemical reactions to form different substances. • A branch of science (a systematic enterprise that builds and organizes knowledge in the form of • Branches of chemistry testable explanations and predictions about the • universe).[1][2][3] Earth science – all-embracing term referring to the fields of science dealing with planet Earth. Earth • A branch of natural science – natural science science is the study of how the natural environ- is a major branch of science that tries to ex- ment (ecosphere or Earth system) works and how it plain and predict nature’s phenomena, based evolved to its current state. -
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T. Crofton Department of Aerospace & Ocean Engineering TEAM LEAD Allison Quinn STUDENT MEMBERS Ethan LeBoeuf Brian McLemore Peter Bradley Smith Amanda Swanson Michael Valosin III Vidya Vishwanathan FACULTY SUPERVISOR AIAA 2018 Undergraduate Spacecraft Design Dr. Kevin Shinpaugh Competition Submission i AIAA Member Numbers and Signatures Ethan LeBoeuf Brian McLemore Member Number: 918782 Member Number: 908372 Allison Quinn Peter Bradley Smith Member Number: 920552 Member Number: 530342 Amanda Swanson Michael Valosin III Member Number: 920793 Member Number: 908465 Vidya Vishwanathan Dr. Kevin Shinpaugh Member Number: 608701 Member Number: 25807 ii Table of Contents List of Figures ................................................................................................................................................................ v List of Tables ................................................................................................................................................................vi List of Symbols ........................................................................................................................................................... vii I. Team Structure ........................................................................................................................................................... 1 II. Introduction .............................................................................................................................................................. -
Appendix I Lunar and Martian Nomenclature
APPENDIX I LUNAR AND MARTIAN NOMENCLATURE LUNAR AND MARTIAN NOMENCLATURE A large number of names of craters and other features on the Moon and Mars, were accepted by the IAU General Assemblies X (Moscow, 1958), XI (Berkeley, 1961), XII (Hamburg, 1964), XIV (Brighton, 1970), and XV (Sydney, 1973). The names were suggested by the appropriate IAU Commissions (16 and 17). In particular the Lunar names accepted at the XIVth and XVth General Assemblies were recommended by the 'Working Group on Lunar Nomenclature' under the Chairmanship of Dr D. H. Menzel. The Martian names were suggested by the 'Working Group on Martian Nomenclature' under the Chairmanship of Dr G. de Vaucouleurs. At the XVth General Assembly a new 'Working Group on Planetary System Nomenclature' was formed (Chairman: Dr P. M. Millman) comprising various Task Groups, one for each particular subject. For further references see: [AU Trans. X, 259-263, 1960; XIB, 236-238, 1962; Xlffi, 203-204, 1966; xnffi, 99-105, 1968; XIVB, 63, 129, 139, 1971; Space Sci. Rev. 12, 136-186, 1971. Because at the recent General Assemblies some small changes, or corrections, were made, the complete list of Lunar and Martian Topographic Features is published here. Table 1 Lunar Craters Abbe 58S,174E Balboa 19N,83W Abbot 6N,55E Baldet 54S, 151W Abel 34S,85E Balmer 20S,70E Abul Wafa 2N,ll7E Banachiewicz 5N,80E Adams 32S,69E Banting 26N,16E Aitken 17S,173E Barbier 248, 158E AI-Biruni 18N,93E Barnard 30S,86E Alden 24S, lllE Barringer 29S,151W Aldrin I.4N,22.1E Bartels 24N,90W Alekhin 68S,131W Becquerei -
Husbandry Guidelines for African Lion Panthera Leo Class
Husbandry Guidelines For (Johns 2006) African Lion Panthera leo Class: Mammalia Felidae Compiler: Annemarie Hillermann Date of Preparation: December 2009 Western Sydney Institute of TAFE, Richmond Course Name: Certificate III Captive Animals Course Number: RUV 30204 Lecturer: Graeme Phipps, Jacki Salkeld, Brad Walker DISCLAIMER The information within this document has been compiled by Annemarie Hillermann from general knowledge and referenced sources. This document is strictly for informational purposes only. The information within this document may be amended or changed at any time by the author. The information has been reviewed by professionals within the industry, however, the author will not be held accountable for any misconstrued information within the document. 2 OCCUPATIONAL HEALTH AND SAFETY RISKS Wildlife facilities must adhere to and abide by the policies and procedures of Occupational Health and Safety legislation. A safe and healthy environment must be provided for the animals, visitors and employees at all times within the workplace. All employees must ensure to maintain and be committed to these regulations of OHS within their workplace. All lions are a DANGEROUS/ HIGH RISK and have the potential of fatally injuring a person. Precautions must be followed when working with lions. Consider reducing any potential risks or hazards, including; Exhibit design considerations – e.g. Ergonomics, Chemical, Physical and Mechanical, Behavioural, Psychological, Communications, Radiation, and Biological requirements. EAPA Standards must be followed for exhibit design. Barrier considerations – e.g. Mesh used for roofing area, moats, brick or masonry, Solid/strong metal caging, gates with locking systems, air-locks, double barriers, electric fencing, feeding dispensers/drop slots and ensuring a den area is incorporated.