Aircraft Contrails Factsheet
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Persistent Contrails and Contrail Cirrus. Part I: Large-Eddy Simulations from Inception to Demise
DECEMBER 2014 L E W E L L E N E T A L . 4399 Persistent Contrails and Contrail Cirrus. Part I: Large-Eddy Simulations from Inception to Demise D. C. LEWELLEN,O.MEZA,* AND W. W. HUEBSCH West Virginia University, Morgantown, West Virginia (Manuscript received 2 October 2013, in final form 10 March 2014) ABSTRACT Large-eddy simulations with size-resolved microphysics are used to model persistent aircraft contrails and contrail-induced cirrus from a few wing spans behind the aircraft until their demise after many hours. Schemes for dynamic local ice binning and updating coupled radiation dynamically as needed in individual columns were developed for numerical efficiency, along with a scheme for maintaining realistic ambient turbulence over long times. These capabilities are used to study some of the critical dynamics involved in contrail evo- lution and to explore the simulation features required for adequate treatment of different components. A ‘‘quasi 3D’’ approach is identified as a useful approximation of the full dynamics, reducing the computation to allow a larger parameter space to be studied. Ice crystal number loss involving competition between different crystal sizes is found to be significant for both young contrails and aging contrail cirrus. As a consequence, the sensitivity to the initial number of ice crystals in the contrail above a threshold is found to decrease signifi- cantly over time, and uncertainties in the ice deposition coefficient and Kelvin effect for ice crystals assume an increased importance. Atmospheric turbulence is found to strongly influence contrail properties and lifetime in some regimes. Water from fuel consumption is found to significantly reduce aircraft-wake-induced ice crystal loss in colder contrails. -
On the Possibility of Weather Modification by Aircraft Contrails
October 1970 745 UDC 651.&€19.6’3:551.576.1:629.135.2(798) ON THE POSSIBILITY OF WEATHER MODIFICATION BY AIRCRAFT CONTRAILS WALLACE B. MURCRAY Geophysical Institute, University of Alaska, College, Alaska ABSTRACT The possible effect of contrails in modifying the weather is reconsidered in the light of information obtained from ground-level contrails in Alaska. It appears likely that inadvertent cloud seeding by jet aircraft may be of the same order of magnitude as that attained in commercial cloud seeding operations. Further investigation is needed; but in the meantime, the possibility of contrail contamination should be kept in mind when evaluating the results of seeding operations. 1. INTRODUCTION frequently such that a contrail is left while the aircraft is taxiing and taking off or landing so that it is easily Aircraft contrails first attracted public attention during accessible for study. (On the ground, the contrail is called World War 11; but as air traffic has built up to its present ice fog, and it can become a serious problem in flight of the environ- level, they have come to be accepted as part operations.) This discussion is based on observations made ment. Even during World War 11, it kas difficult to watch under the direction of Ohtako (1967; see also Huffman the cloud cover laid down by a large bomber formation 1968) during the course of investigations of ice fog from without wondering what it might be doing to the weather; this and other sources. As a result of these observations, at present, there is widespread belief among the general enough is known about the way the contrail is formed to public and some feeling among scientists (Fletcher 1969, make it safe to state that the contrail formed at cruising Reinking 1968, Livingston 1969, and Schaefer 1969) that altitude is very unlikely to differ greatly from that formed contrails are increasing cloudiness, if nothing more, in on the ground. -
Contrails, Contrail Cirrus, and Ship Tracks
214 Proceedings of the TAC-Conference, June 26 to 29, 2006, Oxford, UK Contrails, contrail cirrus, and ship tracks K. Gierens* DLR-Institut für Physik der Atmosphäre Oberpfaffenhofen, Germany Keywords: Aerosol effects on clouds and climate ABSTRACT: The following text is an enlarged version of the conference tutorial lecture on con- trails, contrail cirrus, and ship tracks. I start with a general introduction into aerosol effects on clouds. Contrail formation and persistence, aviation’s share to cirrus trends and ship tracks are treated then. 1 INTRODUCTION The overarching theme above the notions “contrails”, “contrail cirrus”, and “ship tracks” is the ef- fects of anthropogenic aerosol on clouds and on climate via the cloud’s influence on the flow of ra- diation energy in the atmosphere. Aerosol effects are categorised in the following way: - Direct effect: Aerosol particles scatter and absorb solar and terrestrial radiation, that is, they in- terfere directly with the radiative energy flow through the atmosphere (e.g. Haywood and Boucher, 2000). - Semidirect effect: Soot particles are very effective absorbers of radiation. When they absorb ra- diation the ambient air is locally heated. When this happens close to or within clouds, the local heating leads to buoyancy forces, hence overturning motions are induced, altering cloud evolu- tion and potentially lifetimes (e.g. Hansen et al., 1997; Ackerman et al., 2000). - Indirect effects: The most important role of aerosol particles in the atmosphere is their role as condensation and ice nuclei, that is, their role in cloud formation. The addition of aerosol parti- cles to the natural aerosol background changes the formation conditions of clouds, which leads to changes in cloud occurrence frequencies, cloud properties (microphysical, structural, and op- tical), and cloud lifetimes (e.g. -
Video Preview
“ We had only single-seaters. They stood on the wing [and] we were sitting in the cockpit. They showed us everything…, then they said to us, ’this is your speed for take off, and that’s your landing speed… now take off!’ And that’s how we learned to fly it.” --Fran Stigler, Luftwaffe Ace on learning the fly the Me 262 Table of Contents Click the section title to jump to it. Click any blue or purple head to return: Video Preview Video Voices Connect the Video to Science and Engineering Design Explore the Video Explore and Challenge Identify the Challenge Investigate, Compare, and Revise Pushing the Envelope Build Science Literacy through Reading and Writing Summary Activity Next Generation Science Standards Common Core State Standards for ELA & Literacy in Science and Technical Subjects Assessment Rubric For Inquiry Investigation Video Preview "The First Fighter Jet" is one of 20 short videos in the series Chronicles of Courage: Stories of Wartime and Innovation. Introduced in April of 1944, the German Messerschmitt Me 262 was the world’s first jet-powered fighter aircraft. Nicknamed the Schwalbe (Swallow), its twin turbojets were the first ever to be mass produced. The result of innovative research and engineering prowess, the Me 262 could fly faster than its piston engine rivals and was heavily armed. Around 1,400 were built, an insignificant number when compared with the total production runs of almost 34,000 for the Messerschmitt Bf 109 and more than 20,000 for Great Britain’s Supermarine Spitfire. Too few Me 262s arrived too late to change the outcome of World War II. -
The Contrail Mitigation Potential of Aircraft Formation Flight Derived from High-Resolution Simulations
aerospace Article The Contrail Mitigation Potential of Aircraft Formation Flight Derived from High-Resolution Simulations Simon Unterstrasser Deutsches Zentrum für Luft- und Raumfahrt, Institut für Physik der Atmosphäre, Oberpfaffenhofen, 82234 Wessling, Germany; [email protected] Received: 3 November 2020; Accepted: 1 December 2020; Published: 5 December 2020 Abstract: Formation flight is one potential measure to increase the efficiency of aviation. Flying in the upwash region of an aircraft’s wake vortex field is aerodynamically advantageous. It saves fuel and concomitantly reduces the carbon foot print. However, CO2 emissions are only one contribution to the aviation climate impact among several others (contrails, emission of H2O and NOx). In this study, we employ an established large eddy simulation model with a fully coupled particle-based ice microphysics code and simulate the evolution of contrails that were produced behind formations of two aircraft. For a large set of atmospheric scenarios, these contrails are compared to contrails behind single aircraft. In general, contrails grow and spread by the uptake of atmospheric water vapour. When contrails are produced in close proximity (as in the formation scenario), they compete for the available water vapour and mutually inhibit their growth. The simulations demonstrate that the contrail ice mass and total extinction behind a two-aircraft formation are substantially smaller than for a corresponding case with two separate aircraft and contrails. Hence, this first study suggests that establishing formation flight may strongly reduce the contrail climate effect. Keywords: climate impact; aviation; formation flight; mitigation potential; large-eddy simulation LES; particle-based ice microphysics; wake vortex 1. Introduction Formation flight (FF) is a well-known strategy of migratory birds in order to improve their aerodynamic efficiency, save energy and increase their range [1–3]. -
The Jet Generations Photo by Russ Rogers Via Warren Thompson
A 21-year-old RAF pilot and a German graduate student got the whole thing going 70 years ago. The Jet Generations Photo by Russ Rogers via Warren Thompson By Bruce D. Callander N the last months of World War II, was losing the war but was still able self. Within a decade, the propel- Allied bombers were jumped by to inflict damage. ler-driven fighters of the major pow- German interceptors that had no These desperation weapons ar- ers would become virtually obso- propellers but could outrun any rived too late to have any substan- lete, their successors powered by conventional fighter. In the Pa- tial impact on the outcome of the “reaction engines.” cific, the Japanese sent piloted war, but they foreshadowed a post- At the time of the Wright brothers’ Iglide bombs against ships and air- war transformation in military tech- first flight in 1903, a relatively light craft, their suicide dives boosted by nology as dramatic in its way as the internal combustion engine was avail- rocket or turbojet engines. The Axis invention of the flying machine it- able. For the next three decades, pis- A four-ship of F-80 fighters. The Shooting Star was the nation’s first combat jet fighter. 68 AIR FORCE Magazine / October 2002 AIR FORCE Magazine / October 2002 68 A 21-year-old RAF pilot and a German graduate student got the whole thing going 70 years ago. The Jet Generations Photo by Russ Rogers via Warren Thompson By Bruce D. Callander N the last months of World War II, was losing the war but was still able self. -
Community Aspects of Jet Aircraft Noise and Flight Operations
NORC Report: 55A COMMUNITY ASPECTS o F JET A I R CRAFT l\ 0 I S E AND FLIGHT OPERATIONS NATIONAL OPINION RESEARCH CENTER University of Chicago July 1955 " Wright Air Development Center F01mJORD This report was prepared by Paul N. Borsky, Study Director, of the National Opinion Research Center, University of Chicago, under the general direction of Clyde W. Hart, Director of N. C., on Air Force Contract No. AF33(616)-2624, liThe Implications of 1he Opera- tion of Jet Aircraft on Communities in the Vicinity of Airports. It was a.dministered under the direction of the Aero Medical Labora.. tory, Wright Air Development Center, Wright-Patterson Air Force Ba.se, Ohio. Included among those who were primarily responsible for the detailed researoh are David E. Ryan and Richard L. Blumnthal , Assistant study Directors at N. , and Dr. Kenneth N. Stevens of Bolt , Beranek and Newmn Inc. Valuable a.dvice and assistance was also given by Dr. H. O. Parrack, Henig Von Gierke and Captain Ronald Hansen of the Aero Medical Laborato . ... .. .. .... .. .... ... .... ..... ,..... .... ..... ..". ..,... .... .... ..... .. TABLE OF CONTENTS INTRODUCTION. II. FINDINGS II . A. Chronology of Activities. B. Major Problems Considered Relationship of Human Response to Variations of the Airplane Stimulus Importance of Different Parameters of the Airplane StiIn1us. 1\ . 0 a. Variability of sound spectra. b. Variability of peak levels and durations of peak. c. Variability of type of aircraft operation. d. Variability of different typs of airplanes. Variabili ty due to al ti tude of air base and a tmospheric conditions f. Variability due to irregularity of aircraft operations 8: . g. -
How Well Can Persistent Contrails Be Predicted?
aerospace Article How Well Can Persistent Contrails Be Predicted? Klaus Gierens 1,* , Sigrun Matthes 1 and Susanne Rohs 2 1 Deutsches Zentrum für Luft- und Raumfahrt, Institut für Physik der Atmosphäre, D-82234 Oberpfaffenhofen, Germany; [email protected] 2 Forschungszentrum Jülich, IEK-8, D-52425 Jülich, Germany; [email protected] * Correspondence: [email protected] Received: 29 October 2020; Accepted: 27 November 2020 ; Published: 2 December 2020 Abstract: Persistent contrails and contrail cirrus are responsible for a large part of aviation induced radiative forcing. A considerable fraction of their warming effect could be eliminated by diverting only a quite small fraction of flight paths, namely those that produce the highest individual radiative forcing (iRF). In order to make this a viable mitigation strategy it is necessary that aviation weather forecast is able to predict (i) when and where contrails are formed, (ii) which of these are persistent, and (iii) how large the iRF of those contrails would be. Here we study several data bases together with weather data in order to see whether such a forecast would currently be possible. It turns out that the formation of contrails can be predicted with some success, but there are problems to predict contrail persistence. The underlying reason for this is that while the temperature field is quite good in weather prediction and climate simulations with specified dynamics, this is not so for the relative humidity in general and for ice supersaturation in particular. However we find that the weather model shows the dynamical peculiarities that are expected for ice supersaturated regions where strong contrails are indeed found in satellite data. -
Aristo Me 262
A Legacy for the Future: ARISTO ME 262 The pioneers of motorized flight, the Wright Brothers and Charles Lindbergh, lived in the United States of America. But the world’s first usable jet aircraft, the ME 262, was a development of German aircraft builder Professor Dr. Willi Messerschmitt (1898-1978). Bavarian Motor Works, better known as BMW, had made a jet power unit for serial production and gave Messerschmitt the task of building an airplane to accompany the engine. One thousand thirty-three pieces of this revolutionary flying apparatus left Messerschmitt’s workshops starting in 1942. It’s not only its revolutionary engine that makes the ME 262 a classic yet today in aviation technology. Messerschmitt’s engineers created a design of lightness, harmony, and individuality – a design that today is still greatly admired and remains difficult to top. “Beautiful” may not be the appropriate word to describe a mechanism of war, but it is one that certainly applies to the ME 262. Used as a reconnaissance plane, a fighter, and a bomber, the ME 262 was always utilized in new variations toward the end of World War II; in the face of the allied dominance of the skies, however, these jets no longer played an important military role. At the end of the war the Allies’ interest in the ME 262 was great, for at a top speed of more than 870 km/h, it was the fastest airplane of its time. The Americans, the English, and the Russians each secured several flyable pieces for themselves, integrating the ME 262 into their own air forces or using them as schooling aircraft. -
Aircraft Technology Roadmap to 2050 | IATA
Aircraft Technology Roadmap to 2050 NOTICE DISCLAIMER. The information contained in this publication is subject to constant review in the light of changing government requirements and regulations. No subscriber or other reader should act on the basis of any such information without referring to applicable laws and regulations and/or without taking appropriate professional advice. Although every effort has been made to ensure accuracy, the International Air Transport Association shall not be held responsible for any loss or damage caused by errors, omissions, misprints or misinterpretation of the contents hereof. Furthermore, the International Air Transport Association expressly disclaims any and all liability to any person or entity, whether a purchaser of this publication or not, in respect of anything done or omitted, and the consequences of anything done or omitted, by any such person or entity in reliance on the contents of this publication. © International Air Transport Association. All Rights Reserved. No part of this publication may be reproduced, recast, reformatted or transmitted in any form by any means, electronic or mechanical, including photocopying, recording or any information storage and retrieval system, without the prior written permission from: Senior Vice President Member & External Relations International Air Transport Association 33, Route de l’Aéroport 1215 Geneva 15 Airport Switzerland Table of Contents Table of Contents .............................................................................................................................................................................................................. -
Candidate Engines for a Supersonic Business Jet
AIAA Foundation Student Design Competition 2019 - 2020 Undergraduate Team – Engine Candidate Engines for a Supersonic Business Jet Request for Proposal March 10, 2019 2 Abstract New engine designs are solicited for a supersonic business jet that will travel from Europe to North America and back within one business day. Entry into service is expected to be around 2030. The new aircraft must cruise at Mach 1.15 over land, without producing a sonic boom on the ground, but it also must operate at Mach 0.98 in order to offer a cost-per-mile similar to competing subsonic private jets. Over water, it must be possible to cruise at Mach 2.4 and at this speed, with a range 4,600 miles, the aircraft will cross the Atlantic in less than two hours and burn less than 44,000 pounds of fuel. The supersonic business jet is currently powered by two low bypass ratio turbofan engines, each with a nominal net thrust of 21,700 lbf (96.53 kN) at sea level take-off. The challenges of successful commercial operation are quite substantial for any gas turbine engine, however, light weight, low take-off noise, reduced emissions especially at high altitude and affordable fares are paramount. Candidate engines should be lighter than the current power plant and have an improved fuel burn so that the payload and/or operating altitude may be increased and the range may be extended. A generic model of the current power plant is supplied. Responders should generate a typical, multi-segment, mission that addresses the above-listed general improvements specifically and covers design point and off-design engine operations. -
In Situ Observations of Contrail Microphysics and Implications for Their Radiative Impact Michael R
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 104, NO. D10, PAGES 12,077–12,084, MAY 27, 1999 In situ observations of contrail microphysics and implications for their radiative impact Michael R. Poellot Department of Atmospheric Sciences, University of North Dakota, Grand Forks W. Patrick Arnott and John Hallett Atmospheric Science Center, Desert Research Institute, Reno, Nevada Abstract. In this study we present the microphysical characteristics of 21 jet contrail clouds sampled in situ and examine the possible effects of exhaust on natural cirrus and radiative effects of contrails. Microphysical samples were obtained with Particle Measuring Systems (PMS) 2D-C, 1D-C, and FSSP probes. About one half of the study contrails were generated by the sampling aircraft, a Cessna Citation, primarily at times of 3–15 min after generation; the source and age of the others is unknown. On average, the contrails contained particles of mean diameter of the order of 10 mm in concentrations exceeding 2 10,000 L 1. Contrails embedded in natural cirrus appeared to have little effect on the natural cloud microphysics. Anomalous diffraction theory was used to model radiative properties of sampled contrails. The contrail cirrus showed considerably more spectral variation in extinction and absorption efficiencies than natural cirrus because of the large numbers of small crystals in contrails. Embedded contrails also displayed greater emissivity and emission than natural cirrus and a greater spectral variation in transmission. 1. Introduction Illinois also showed locally significant radiative effects [Wend- land and Semonin, 1982]. The radiative impact of an aircraft Increasing levels of air traffic have raised concerns about the contrail is dependent to a large degree on the cloud micro- potential effects of aircraft exhaust on the climate.