Physics of Meteor Generated Shock Waves in the Earth's Atmosphere
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Report of the Commission on the Scientific Case for Human Space Exploration
1 ROYAL ASTRONOMICAL SOCIETY Burlington House, Piccadilly London W1J 0BQ, UK T: 020 7734 4582/ 3307 F: 020 7494 0166 [email protected] www.ras.org.uk Registered Charity 226545 Report of the Commission on the Scientific Case for Human Space Exploration Professor Frank Close, OBE Dr John Dudeney, OBE Professor Ken Pounds, CBE FRS 2 Contents (A) Executive Summary 3 (B) The Formation and Membership of the Commission 6 (C) The Terms of Reference 7 (D) Summary of the activities/meetings of the Commission 8 (E) The need for a wider context 8 (E1) The Wider Science Context (E2) Public inspiration, outreach and educational Context (E3) The Commercial/Industrial context (E4) The Political and International context. (F) Planetary Science on the Moon & Mars 13 (G) Astronomy from the Moon 15 (H) Human or Robotic Explorers 15 (I) Costs and Funding issues 19 (J) The Technological Challenge 20 (J1) Launcher Capabilities (J2) Radiation (K) Summary 23 (L) Acknowledgements 23 (M) Appendices: Appendix 1 Expert witnesses consulted & contributions received 24 Appendix 2 Poll of UK Astronomers 25 Appendix 3 Poll of Public Attitudes 26 Appendix 4 Selected Web Sites 27 3 (A) Executive Summary 1. Scientific missions to the Moon and Mars will address questions of profound interest to the human race. These include: the origins and history of the solar system; whether life is unique to Earth; and how life on Earth began. If our close neighbour, Mars, is found to be devoid of life, important lessons may be learned regarding the future of our own planet. 2. While the exploration of the Moon and Mars can and is being addressed by unmanned missions we have concluded that the capabilities of robotic spacecraft will fall well short of those of human explorers for the foreseeable future. -
Forthcoming Changes in the Global Satellite Observing Systems Mitch Goldberg, NOAA Outline
Forthcoming changes in the Global Satellite Observing Systems Mitch Goldberg, NOAA Outline Overview of CGMS and CEOS. Overview of the key satellite observations for NWP Discuss satellite agencies plans for these key observations Short overview emerging observations or technology which we need to pay attention to. Summary Members: CMA CNES CNSA ESA EUMETSAT IMD IOC/UNESCO JAXA JMA KMA NASA ROSCOSMOS ROSHYRDOMET WMO Observers: CSA EC ISRO KARI KORDI SOA Strategy for addressing key satellite data Begin with WIGOS 5th Workshop of the Impact of Various Observing Systems on NWP (Sedona Report). UKMO impact report: Impact of Metop and other satellite data within the Met Office global NWP system using a forecast adjoint-based sensitivity method- Feb 2012, tech repot #562 and MWR October 2013 paper Recall key observation types for NWP Compare with what space agencies are planning to provide continuity and enhancements to these observing types. Make use of the WMO OSCAR database Time scale between now and 2030. Sedona Report Observations contributing to the largest reduction of forecast errors are those observations with vertical information (temperature, water vapor). The single instrument with the largest impact is hyperspectral IR Microwave dominates because of the number of satellites and ability to view thru low water content clouds. However, there is now no single, dominating satellite sensor. GPSRO shows good impact, and largest impact per observation Atmospheric Motion Vector Winds and Scatterometers are single level data and have modest impacts Concerns about the declining number of observations into the future – mostly due to the replacement of 2 year life satellites with 7 years (e.g. -
Radio Emissions Associated with Shock Waves and a Brief Model of Type Ii Solar Radio Bursts
RADIO EMISSIONS ASSOCIATED WITH SHOCK WAVES AND A BRIEF MODEL OF TYPE II SOLAR RADIO BURSTS C. S. Wu¤ Abstract In this paper, we discuss the generation of radio waves at shock waves. Two cases are considered. One is associated with a quasi{perpendicular shock and the other is with a quasi{parallel shock. In the former case, it is stressed that a nearly perpendicular shock can lead to a fast Fermi acceleration. Looking at these energized electrons either in the deHo®mann{Teller frame or the plasma frame, one concludes that the accelerated electrons should inherently possess a loss{cone distribution after the mirror reflection at the shock. Consequently, these electrons can lead to induced emission of radio waves via a maser instability. In the latter case, we assume that a quasi{parallel shock is propagating in an environment which has already been populated with energetic electrons. In this case, the shock wave can also lead to induced radiation via a maser instability. Based on this notion, we describe briefly a model to explain the Type II solar radio bursts which is a very intriguing phenomenon and has a long history. 1 Introduction An interesting theoretical issue is how radio emission processes can be induced or triggered by shock waves under various physical conditions. In this article, we present a discussion which comprises two parts. The ¯rst part is concerned with a nearly perpendicular shock. In this case, the shock can energize a fraction of the thermal electrons or suprathermal electrons to much higher energies by means of a fast Fermi process. -
Analysis of Flow Structures in Wake Flows for Train Aerodynamics Tomas W. Muld
Analysis of Flow Structures in Wake Flows for Train Aerodynamics by Tomas W. Muld May 2010 Technical Reports Royal Institute of Technology Department of Mechanics SE-100 44 Stockholm, Sweden Akademisk avhandling som med tillst˚and av Kungliga Tekniska H¨ogskolan i Stockholm framl¨agges till offentlig granskning f¨or avl¨aggande av teknologie licentiatsexamen fredagen den 28 maj 2010 kl 13.15 i sal MWL74, Kungliga Tekniska H¨ogskolan, Teknikringen 8, Stockholm. c Tomas W. Muld 2010 Universitetsservice US–AB, Stockholm 2010 Till Mamma ♥ iii iv The Only Easy Day Was Yesterday Motto of the United States Navy SEALs Aerodynamics are for people who can’t build engines Enzo Ferrari v Analysis of Flow Structures in Wake Flows for Train Aero- dynamics Tomas W. Muld Linn´eFlow Centre, KTH Mechanics, Royal Institute of Technology SE-100 44 Stockholm, Sweden Abstract Train transportation is a vital part of the transportation system of today and due to its safe and environmental friendly concept it will be even more impor- tant in the future. The speeds of trains have increased continuously and with higher speeds the aerodynamic effects become even more important. One aero- dynamic effect that is of vital importance for passengers’ and track workers’ safety is slipstream, i.e. the flow that is dragged by the train. Earlier ex- perimental studies have found that for high-speed passenger trains the largest slipstream velocities occur in the wake. Therefore the work in this thesis is devoted to wake flows. First a test case, a surface-mounted cube, is simulated to test the analysis methodology that is later applied to a train geometry, the Aerodynamic Train Model (ATM). -
A Review of Wind Turbine Wake Models and Future Directions
A Review of Wind Turbine Wake Models and Future Directions 2013 North American Wind Energy Academy (NAWEA) Symposium Matthew J. Churchfield Boulder, Colorado August 6, 2013 NREL/PR-5200-60208 NREL is a national laboratory of the U.S. Department of Energy, Office of Energy Efficiency and Renewable Energy, operated by the Alliance for Sustainable Energy, LLC. Why Are Wind Turbine Wakes Important? Wind speed (m/s) • Wake effects impact: o Power production o Mechanical loads • High importance in wind- plant-level control strategies • Having a good wake model is a necessity in predicting plant performance and understanding fatigue Contours of instantaneous wind speed in simulated flow through loads the Lillgrund wind plant 2 What Does a Wake Look Like? Flow field generated from large-eddy simulation (velocity field minus mean shear) top view Characteristics: • Velocity deficit • Low-frequency meandering • Intermittent edge • Shear-layer-generated turbulence view from downstream Notice how many of the characteristics describe some sort of unsteadiness 3 Differing Needs in Wake Modeling • Power Prediction and Annual Energy Production (AEP) o Steady, time-averaged • Loads o Unsteady, time-accurate • Control Strategies o Steady and unsteady may both be needed • Basic Physics o As much fidelity as possible 4 Hierarchy of Wake Models Type Example Empirical -Jensen (1983)/Katíc (1986) (Park) Linearized -Ainslie (1985) (Eddy-viscosity) i Reynolds-averaged -Ott et al. (2011) (Fuga) ncreasing cost/fidelity Navier-Stokes (RANS) Other -Larsen et al. (2007) -
The Kelvin Wedge
The shape of ship wakes: The Kelvin wedge 1 1 o 2sin 3 38.9 Dr Andrew French. August 2013 1 Contents • Ship wakes and the Kelvin wedge • Theory of surface waves – Frequency – Wavenumber – Dispersion relationship – Phase and group velocity – Shallow and deep water waves – Minimum velocity of deep water ripples • Mathematical derivation of Kelvin wedge – Surf-riding condition – Stationary phase – Rabaud and Moisy’s model – Froude number • Minimum ship speed needed to generate a Kelvin wedge • Kelvin wedge via a geometrical method? – Mach’s construction • Further reading 2 A wake is an interference pattern of waves formed by the motion of a body through a fluid. Intriguingly, the angular width of the wake produced by ships (and ducks!) in deep water is the same (about 38.9o). A mathematical explanation for this phenomenon was first proposed by Lord Kelvin (1824-1907). The triangular envelope of the wake pattern has since been known as the Kelvin wedge. http://en.wikipedia.org/wiki/Wake 3 Venetian water-craft and their associated Kelvin wedges Images from Google Maps (above) and Google Earth (right), (August 2013) 4 Still awake? 5 The Kelvin Wedge is clearly not the whole story, it merely describes the envelope of the wake. Other distinct features are highlighted below: Turbulent Within the Kelvin wedge we flow from bow see waves inclined at a wave and slightly wider angle propeller from the direction of travel of wash. * These the ship. (It turns effects will be out this is about 55o) * addressed in this presentation. The others Waves disperse within a ‘few will not! degrees’ of the Kelvin wedge. -
Fred Mistichelli NESDIS Spectrum Manager Rich Kelley Alion Science
WRC-19 Fred Mistichelli Geneva NESDIS Spectrum Manager 28 October to 22 November 2019 Rich Kelley Alion Science for NESDIS 29 Nov – 5 Dec 2017 o discusses spectrum concerns faced by ITSC membership between now and 2019. o covers WRC- 19 agenda items of concern in passive bands and one major new active downlink o describes rfi detection and suppression methods Satellites and agencies possibly affected by WRC-19 decisions Satellite agency Satellite agency Aqua NASA Meteor-M N2 RosHydroMet Coriolis DoD Meteor-M N2-1 RosHydroMet DWSS-1 DoD Meteor-M N2-2 RosHydroMet DWSS-2 DoD Meteor-M N2-3 RosHydroMet FY-3B CMA Meteor-M N2-4 RosHydroMet FY-3C CMA Meteor-M N2-5 RosHydroMet FY-3D CMA Meteor-MP N1 RosHydroMet FY-3E CMA Meteor-MP N2 RosHydroMet FY-3F CMA Metop-A EUMETSAT FY-3G CMA Metop-B EUMETSAT FY-3H CMA Metop-C EUMETSAT FY-3RM-1 CMA Metop-SG-A1 EUMETSAT FY-3RM-2 CMA Metop-SG-A2 EUMETSAT GCOM-W1 JAXA Metop-SG-A3 EUMETSAT GPM Core Observatory NASA Metop-SG-B1 EUMETSAT HY-2A NSOAS Metop-SG-B2 EUMETSAT JPSS-1 NOAA Metop-SG-B3 EUMETSAT JPSS-2 NOAA NOAA-15 NOAA JPSS-3 NOAA NOAA-18 NOAA JPSS-4 NOAA NOAA-19 NOAA Megha-Tropiques ISRO SNPP NOAA [1] National Ocean Satellite Application Center (China) Agenda item spectrum addressed 1.5 17.7-19.7 GHz (space-to-Earth) and 27.5-29.5 GHz (Earth-to-space) 1.6 37.5-39.5 GHz (space-to-Earth), 39.5-42.5 GHz (space-to-Earth), 47.2-50.2 GHz (Earth-to-space) and 50.4-51.4 GHz (Earth-to-space) 1.7 spectrum requirements for telemetry, tracking and command in the space operation service for the growing number of non-GSO satellites with short duration missions (small satellites/microsats/picosats) 1.13 24.25-27.5 GHz (data downlink for JPSS/MetOp) 31.8-33.4 GHz 37-40.5 GHz 47.2-50.2 GHz (passive use only) 50.4-52.6 GHz (passive use only) 81-86 GHz 1.14 regulatory actions for high-altitude platform stations (HAPS), within existing fixed-service allocations Issue 9.1.9 51.4-52.4 GHz n.b.The WMO position paper on WRC 19 agenda items is at (http://wis.wmo.int/file=3379). -
Formation Mechanisms of Ringwoodite: Clues from the Martian Meteorite
Zhang et al. Earth, Planets and Space (2021) 73:165 https://doi.org/10.1186/s40623-021-01494-1 FULL PAPER Open Access Formation mechanisms of ringwoodite: clues from the Martian meteorite Northwest Africa 8705 Ting Zhang1,2, Sen Hu1, Nian Wang1,2, Yangting Lin1* , Lixin Gu1,3, Xu Tang1,3, Xinyu Zou4 and Mingming Zhang1 Abstract Ringwoodite and wadsleyite are the high-pressure polymorphs of olivine, which are common in shocked meteorites. They are the major constituent minerals in the terrestrial mantle. NWA 8705, an olivine-phyric shergottite, was heavily shocked, producing shock-induced melt veins and pockets associated with four occurrences of ringwoodite: (1) the lamellae intergrown with the host olivine adjacent to a shock-induced melt pocket; (2) polycrystalline assemblages preserving the shapes and compositions of the pre-existing olivine within a shock-induced melt vein (60 μm in width); (3) the rod-like grains coexisting with wadsleyite and clinopyroxene within a shock-induced melt vein; (4) the microlite clusters embedded in silicate glass within a very thin shock-induced melt vein (20 μm in width). The frst two occurrences of ringwoodite likely formed via solid-state transformation from olivine, supported by their mor- phological features and homogeneous compositions (Mg# 64–62) similar to the host olivine (Mg# 66–64). The third occurrence of ringwoodite might fractionally crystallize from the shock-induced melt, based on its heterogeneous and more FeO-enriched compositions (Mg# 76–51) than those of the coexisting wadsleyite (Mg# 77–67) and the host olivine (Mg# 66–64) of this meteorite. The coexistence of ringwoodite, wadsleyite, and clinopyroxene suggests a post- shock pressure of 14–16 GPa and a temperature of 1650–1750 °C. -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
What Is a Quantum Shock Wave?
What is a quantum shock wave? S. A. Simmons,1 F. A. Bayocboc, Jr.,1 J. C. Pillay,1 D. Colas,1, 2 I. P. McCulloch,1 and K. V. Kheruntsyan1 1School of Mathematics and Physics, University of Queensland, Brisbane, Queensland 4072, Australia 2ARC Centre of Excellence in Future Low-Energy Electronics Technologies, University of Queensland, Brisbane, Queensland 4072, Australia (Dated: November 4, 2020) Shock waves are examples of the far-from-equilibrium behaviour of matter; they are ubiquitous in nature, yet the underlying microscopic mechanisms behind their formation are not well understood. Here, we study the dynamics of dispersive quantum shock waves in a one-dimensional Bose gas, and show that the oscillatory train forming from a local density bump expanding into a uniform background is a result of quantum mechanical self- interference. The amplitude of oscillations, i.e., the interference contrast, decreases with the increase of both the temperature of the gas and the interaction strength due to the reduced phase coherence length. Furthermore, we show that vacuum and thermal fluctuations can significantly wash out the interference contrast, seen in the mean-field approaches, due to shot-to-shot fluctuations in the position of interference fringes around the mean. Introduction.—The study of dispersive shock waves in linear interaction [22], in both the GPE and NLSE, has been superfluids, such as dilute gas Bose-Einstein condensates exploited in, and is required for, the interpretation of disper- (BECs), has been attracting a growing attention in recent years sive shock waves as a train of grey solitons [6, 23]. However, (see, e.g., Refs. -
Handbook of Iron Meteorites, Volume 2 (Bitburg
326 Bishop Canyon - Bitburg fibrous and brecciated, and 1-100 p wide veins through it ' l ' j are filled with a glass in which silicate fragments and a little ) ·. / troilite are embedded.lt is surprising to note how the shock . e·· f . has been able to create such heavy local transformation; 10 mm away nothing unusual is observed. The local damage resembles in several respects the structural changes associated with spot welding. Examination under the electron microprobe suggests that the unknown silicate is ~' almost pure Si02 , possibly tridymite. Bishop Canyon is chemically and structurally a typical ~ phosphorus-poor, fine octahedrite of groupiVA, . l .. resembling in particular Gibe on. It is, however, unusual in .0 its silicate inclusions, the shock damage and low hardness. ,, .• ~: :t • ·. • cr ··. @ Specimen in the U.S. National Museum in Washington: .. ~ - ,·r -. f '-' f 226 g slice (no. 770, 9.5 x 4.5 x 0.9 em) II . 0 t' / •. ' ~~ ~~ {) r ...~ · -· · ...· ~· -/~... Figure 352. Bitburg. Detail of Figure 350. The dendritic metal was Bitburg, Rhineland, Germany at high temperature austenite but transformed upon cooling to unequilibrated a • Etched. Scale bar 50 f.l. 49°58'N, 6°32'E 2 A mass said to have weighed 1.5 tons was smelted in a furnace before 1805. It was recognized as a meteorite (Chladni 1819: 353), but virtually nothing was saved of the undamaged material (Hey 1966: 57). The smelted material, e.g., no. 1881, 1534 of 546 gin .. \ . • I : '/ 'I \ ' . ~\.. // .·· Figure 350. Bit burg (Copenhagen no. 1886, 493). A rectangular bar cut from melted material of the Bitburg meteorite. -
Radar-Enabled Recovery of the Sutter's Mill Meteorite, A
RESEARCH ARTICLES the area (2). One meteorite fell at Sutter’sMill (SM), the gold discovery site that initiated the California Gold Rush. Two months after the fall, Radar-Enabled Recovery of the Sutter’s SM find numbers were assigned to the 77 me- teorites listed in table S3 (3), with a total mass of 943 g. The biggest meteorite is 205 g. Mill Meteorite, a Carbonaceous This is a tiny fraction of the pre-atmospheric mass, based on the kinetic energy derived from Chondrite Regolith Breccia infrasound records. Eyewitnesses reported hearing aloudboomfollowedbyadeeprumble.Infra- Peter Jenniskens,1,2* Marc D. Fries,3 Qing-Zhu Yin,4 Michael Zolensky,5 Alexander N. Krot,6 sound signals (table S2A) at stations I57US and 2 2 7 8 8,9 Scott A. Sandford, Derek Sears, Robert Beauford, Denton S. Ebel, Jon M. Friedrich, I56US of the International Monitoring System 6 4 4 10 Kazuhide Nagashima, Josh Wimpenny, Akane Yamakawa, Kunihiko Nishiizumi, (4), located ~770 and ~1080 km from the source, 11 12 10 13 Yasunori Hamajima, Marc W. Caffee, Kees C. Welten, Matthias Laubenstein, are consistent with stratospherically ducted ar- 14,15 14 14,15 16 Andrew M. Davis, Steven B. Simon, Philipp R. Heck, Edward D. Young, rivals (5). The combined average periods of all 17 18 18 19 20 Issaku E. Kohl, Mark H. Thiemens, Morgan H. Nunn, Takashi Mikouchi, Kenji Hagiya, phase-aligned stacked waveforms at each station 21 22 22 22 23 Kazumasa Ohsumi, Thomas A. Cahill, Jonathan A. Lawton, David Barnes, Andrew Steele, of 7.6 s correspond to a mean source energy of 24 4 24 2 25 Pierre Rochette, Kenneth L.