University of Birmingham Aircraft Engine Exhaust Emissions And
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Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
2. Afterburners
2. AFTERBURNERS 2.1 Introduction The simple gas turbine cycle can be designed to have good performance characteristics at a particular operating or design point. However, a particu lar engine does not have the capability of producing a good performance for large ranges of thrust, an inflexibility that can lead to problems when the flight program for a particular vehicle is considered. For example, many airplanes require a larger thrust during takeoff and acceleration than they do at a cruise condition. Thus, if the engine is sized for takeoff and has its design point at this condition, the engine will be too large at cruise. The vehicle performance will be penalized at cruise for the poor off-design point operation of the engine components and for the larger weight of the engine. Similar problems arise when supersonic cruise vehicles are considered. The afterburning gas turbine cycle was an early attempt to avoid some of these problems. Afterburners or augmentation devices were first added to aircraft gas turbine engines to increase their thrust during takeoff or brief periods of acceleration and supersonic flight. The devices make use of the fact that, in a gas turbine engine, the maximum gas temperature at the turbine inlet is limited by structural considerations to values less than half the adiabatic flame temperature at the stoichiometric fuel-air ratio. As a result, the gas leaving the turbine contains most of its original concentration of oxygen. This oxygen can be burned with additional fuel in a secondary combustion chamber located downstream of the turbine where temperature constraints are relaxed. -
A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport
University of New Hampshire University of New Hampshire Scholars' Repository Applied Engineering and Sciences Scholarship Applied Engineering and Sciences 8-22-1985 A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport Theodore S. Tavares University of New Hampshire, Manchester, [email protected] Follow this and additional works at: https://scholars.unh.edu/unhmcis_facpub Recommended Citation Tavares, T.S., “A Supersonic Fan Equipped Variable Cycle Engine for a Mach 2.7 Supersonic Transport,” NASA-CR-177141, 1986. This Report is brought to you for free and open access by the Applied Engineering and Sciences at University of New Hampshire Scholars' Repository. It has been accepted for inclusion in Applied Engineering and Sciences Scholarship by an authorized administrator of University of New Hampshire Scholars' Repository. For more information, please contact [email protected]. https://ntrs.nasa.gov/search.jsp?R=19860019474 2018-07-25T19:53:49+00:00Z ^4/>*>?/ GAS TURBINE LABORATORY DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS MASSACHUSETTS INSTITUTE OF TECHNOLOGY CAMBRIDGE, MA 02139 A FINAL REPORT ON NASA GRANT NAG-3-697 entitled A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A MACH 2.7 SUPERSONIC TRANSPORT by T. S. Tavares prepared for NASA Lewis Research Center Cleveland, OH 44135 (NASA-CB-177141) A SDPEBSCNIC FAN EQUIPPED N86-28946 VARIABLE CYCLE ENGINE.JOB A MACH 2.? SDPEESONIC TBANSPOBT Final Report (Massachusetts Inst. of Tech.) 107 p Unclas CSCL 21E G3/07 43461 August 22, 1985 A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A HACK 2.7 SUPERSONIC TRANSPORT by Theodore Sean Tavares A SUPERSONIC FAN EQUIPPED VARIABLE CYCLE ENGINE FOR A MACH 2.7 SUPERSONIC TRANSPORT by THEODORE SEAN TAVARES ABSTRACT A design stud/ was carried out to evaluate the concept of a variable cycle turbofan engine with an axially supersonic fan stage as powerplant for a Mach 2.7 supersonic transport. -
Implementation of a Random Forest Classifier to Examine Wildfire Predictive Modeling in Greece Using Diachronically Collected Fire Occurrence and Fire Mapping Data
Implementation of a Random Forest classifier to examine wildfire predictive modeling in Greece using diachronically collected fire occurrence and fire mapping data Authors: Alex Apostolakis, Stella Girtsou, Charalampos Kontoes, Ioannis Papoutsis, Michalis Tsoutsos e-mails: {alex.apostolakis, sgirtsou, kontoes, ipapoutsis, mtsoutsos}@noa.gr Beyond center of excelence, IAASARS, National Observatory of Athens, Greece Presenter: Alex Apostolakis Recent Forest fire disasters 2019 Bush fires in New South Wales of Australia burned about 1.65 million hectares 2019 Brazilian Space Agency has reported an 83% increase in fire occurrences compared to the same period of the previous year. 2018 Attica wildfires spread up to a speed of 124 km/h resulting to more than a hundred casualties. Climate change impact The problem of the wildfires becomes considerably important if we account for the climate change scenarios which suggest substantial warming and increase of heat waves, drought and dry spell events across the entire Mediterranean in the future years. Model categories for fire risk prediction Theoretical (or physics-based) : Theoretical models are entirely based on equations that describe the physics of the related to the fire ignition physical phenomena like fluid mechanics, combustion and heat transfer Data-driven models : Data-driven models (also known as empirical models before the data science developments) are purely based on the correlations between data extracted from historical fire records and their related parameters. Machine learning models belong to this category. Why Machine Learning models Machine Learning algorithms are designed to automatically formulate the complex mathematical relations between the input parameters. In Physical-based models the mathematics of those relations should be known in advance. -
Disaster Preparedness, Resilience, and Response Forum Report
Columbia World Projects: Disaster Preparedness, Resilience, and Response Forum Report August 15, 2019 Foreword Dear Reader, On behalf of Columbia World Projects (CWP), we are pleased to present the following report on our Forum on Disaster Preparedness, Resilience, and Response, one of an ongoing series of meetings dedicated to bringing together academia with partners from government, non- governmental and intergovernmental organizations, the media, and the private sector to identify projects designed to tackle fundamental challenges facing humanity. Natural disasters and public health emergencies impact tens of millions of people each year. At the individual level, the impact is often felt physically, mentally, and emotionally, and can destroy homes and businesses, wipe out financial resources, uproot families, and cause lasting injuries and even deaths. At the community and regional level, the impact can be equally devastating, inflicting enormous environmental and structural damage; stalling or even reversing a society’s economic growth and development; and producing and exacerbating poverty and instability. While natural disasters and public health emergencies have been a consistent feature of human existence, the frequency and intensity of such incidents have increased over the last few decades, in significant part as a result of climate change and growing mobility. All of this has made managing disasters more urgent, more expensive, and more complex. On June 10, 2019, CWP invited approximately 35 experts from a range of fields and disciplines to take part in a Forum with the aim not only of deepening our understanding of natural disasters and public health emergencies, but also of proposing concrete ways to improve the lives of people affected by these events. -
Wildfire Management in Europe Final Report and Recommendation Paper Cmine Task Group Wildfire
WILDFIRE MANAGEMENT IN EUROPE FINAL REPORT AND RECOMMENDATION PAPER CMINE TASK GROUP WILDFIRE The final output of the one-year mandate of the CMINE Wildfire Task Group work is a recommendation to align EU legislation and national, regional and local levels of governance regarding land management to facilitate the mitigation of the risks of wildfires.. Nina Dobrinkova, Bulgarian Academy of Sciences (IICT-BAS) February 2020 TABLE OF CONTENTS EXECUTIVE SUMMARY ................................................................................................................................. 3 ACKNOWLEDGEMENTS .............................................................................................................................. 4 INTRODUCTION ........................................................................................................................................... 7 CONTEXT OF THE TASK GROUP ........................................................................................................................... 7 GOAL OF THE TASK GROUP .................................................................................................................................. 7 EUROPEAN FIRES 'STATE OF THE ART' .............................................................................................................. 8 GENERAL INFORMATION ON WILDFIRES ........................................................................................................ 9 WILDFIRE CHARACTERISATION ........................................................................................................................ -
Sorli Fil1l1ivffisfifiy ...I
\;11 ttl I / ~ sorlI fil1l1IVffiSfifiY ...i ......._---------------- -- - United States Department of Fire Agriculture Forest Service Management S An international quarterly periodical Volume 50, NO.1 Notes devoted to forest fire management 1989 Contents 2 Fire Management: Strength Through Diversity 53 Forest Fire Simulation Video and Graphic System Harry Croft L.F. Southard 6 Major Transitions in Firefighting: 1950 to 1990 56 Smoke Management Modeling in the Bureau of Jack F. Wilson Land Management Allen R. Riebau and Michael L. Sestak 9 A Look at the Next 50 Years John R. Warren 59 Smoke From Smoldering Fires-a Road Hazard Leonidas G. Lavdas 13 Warm Springs Hotshots Holly M. Gill 63 Author Index-Volume 49 16 Wildfire Law Enforcement-Virginia Style 65 Subject Index-Volume 49 John N. Graff 19 Fire Management in the Berkeley Hills Short Features Carol L. Rice, 1 Thank you, Fire Management Notes 21 Light-Hand Suppression Tactics-a Fire Allan J West Management Challenge Francis Mohr 5 Workforce Diversity-What We Can Do! L.A. Amicare//a 31 Lightning Fires in Saskatchewan Forests c.i Oglivie 8 The Fire Equipment Working Team William Shenk 37 GSA-a Partner in Wildfire Protection 11 Smokejumper Reunion-June 1989 Larry Camp Janice Eberhardt 38 Predicting Fire Potential 15 NWCG's Publication Management System: Thomas J. Rios A Progress Report Mike Munkres 42 Wildfire 1988-a Year To Remember Arnold F. Hartigan 55 Identifying Federal Excess Personal Property Francis R. Russ 45 Documenting Wildfire Behavior: The 1988 Brereton Lake Fire, Manitoba Kelvin G. Hirsch Special Features 49 Fire Observation Exercises-a Valuable Part of 24 The Way Wc Were Fire Behavior Training Patricia L. -
04 Propulsion
Aircraft Design Lecture 2: Aircraft Propulsion G. Dimitriadis and O. Léonard APRI0004-1, Aerospace Design Project, Lecture 4 1 Introduction • A large variety of propulsion methods have been used from the very start of the aerospace era: – No propulsion (balloons, gliders) – Muscle (mostly failed) – Steam power (mostly failed) – Piston engines and propellers – Rocket engines – Jet engines – Pulse jet engines – Ramjet – Scramjet APRI0004-1, Aerospace Design Project, Lecture 4 2 Gliding flight • People have been gliding from the- mid 18th century. The Albatross II by Jean Marie Le Bris- 1849 Otto Lillienthal , 1895 APRI0004-1, Aerospace Design Project, Lecture 4 3 Human-powered flight • Early attempts were less than successful but better results were obtained from the 1960s onwards. Gerhardt Cycleplane (1923) MIT Daedalus (1988) APRI0004-1, Aerospace Design Project, Lecture 4 4 Steam powered aircraft • Mostly dirigibles, unpiloted flying models and early aircraft Clément Ader Avion III (two 30hp steam engines, 1897) Giffard dirigible (1852) APRI0004-1, Aerospace Design Project, Lecture 4 5 Engine requirements • A good aircraft engine is characterized by: – Enough power to fulfill the mission • Take-off, climb, cruise etc. – Low weight • High weight increases the necessary lift and therefore the drag. – High efficiency • Low efficiency increases the amount fuel required and therefore the weight and therefore the drag. – High reliability – Ease of maintenance APRI0004-1, Aerospace Design Project, Lecture 4 6 Piston engines • Wright Flyer: One engine driving two counter- rotating propellers (one port one starboard) via chains. – Four in-line cylinders – Power: 12hp – Weight: 77 kg APRI0004-1, Aerospace Design Project, Lecture 4 7 Piston engine development • During the first half of the 20th century there was considerable development of piston engines. -
First Main Title Line First Line Forest Fires in Europe, Middle East and North Africa 2014
First Main Title Line First Line Forest Fires in Europe, Middle East and North Africa 2014 Joint report of JRC and Directorate-General Environment 2015 Report EUR 27400 EN European Commission Joint Research Centre Institute for Environment and Sustainability Contact information San-Miguel- Ayanz Jesús Address: Joint Research Centre, Via Enrico Fermi 2749, TP 261, 21027 Ispra (VA), Italy E-mail: [email protected] Tel.: +39 0332 78 6138 JRC Science Hub https://ec.europa.eu/jrc Legal Notice This publication is a Technical Report by the Joint Research Centre, the European Commission’s in-house science service. It aims to provide evidence-based scientific support to the European policy-making process. The scientific output expressed does not imply a policy position of the European Commission. Neither the European Commission nor any person acting on behalf of the Commission is responsible for the use which might be made of this publication. All images © European Union 2015 JRC97214 EUR 27400 EN ISBN 978-92-79-50447-1 (PDF) ISBN 978-92-79-50446-4 (print) ISSN 1831-9424 (online) ISSN 1018-5593 (print) doi:10.2788/224527 Luxembourg: Publications Office of the European Union, 2015 © European Union, 2015 Reproduction is authorised provided the source is acknowledged. Abstract This is the 15th issue of the EFFIS annual report on forest fires for the year 2014. This report is consolidated as highly appreciated documentation of the previous year's forest fires in Europe, Middle East and North Africa. In its different sections, the report includes information on the evolution of fire danger in the European and Mediterranean regions, the damage caused by fires and detailed description of the fire conditions during the 2014 fire campaign in the majority of countries in the EFFIS network The chapter on national reporting gives an overview of the efforts undertaken at national and regional levels, and provides inspiration for countries exposed to forest fire risk. -
An Online Performance Calculator for Ramjet, Turbojet, Turbofan, and Turboprop Engines
An Online Performance Calculator for Ramjet, Turbojet, Turbofan, and Turboprop Engines Evan P. Warner∗ Virginia Tech, Blacksburg, VA, 24061, USA This paper documents the theory, equations, and assumptions behind an HTML-based online performance calculator for ramjet, turbojet, turbofan, and turboprop engines. Based on inputs of design parameters, flight con- ditions, and engine parameters, the specific thrust (()), thrust specific fuel consumption ()(), propulsive efficiency ([ ?), thermal efficiency ([Cℎ), and overall efficiency ([0) will be output for the engine of interest. Several sample cases are analyzed to verify the functionality of the calculator. These sample cases are derived from engines associated with Virginia Tech, which include: Pratt & Whitney’s PT6A-20 and JT15D-1, Honeywell’s TFE731-2B, and the Rolls Royce Trent 1000. With the help of this calculator, students will now be able to verify their air-breathing jet engine performance value calculations. This calculator is available here. I. Nomenclature "0 = Ambient Mach Number 2 ?1 = Specific Heat of the Burner W0 = Ambient Specific Heat Ratio 2 ?C = Specific Heat of the Turbine W3 = Diffuser Specific Heat Ratio 2 ? 5 = Specific Heat of the Fan W2 = Compressor Specific Heat Ratio )0 = Ambient Static Temperature W1 = Burner Specific Heat Ratio ?0 = Ambient Static Pressure WC = Turbine Specific Heat Ratio ?4 = Exit Static Pressure W= = Nozzle Specific Heat Ratio '08A = Gas Constant for Air W 5 = Fan Specific Heat Ratio '?A>3 = Gas Constant for the Products of Fuel/Air Mixture W= 5 = Fan Nozzle -
Modelling and Simulation of the Revolutionary Turbine Accelerator
Announcement “This final year project was an exam. Commentary made during the presentation is not taken into account.” "Deze eindverhandeling was een examen. De tijdens de verdediging geformuleerde opmerkingen werden niet opgenomen". Preface Here I would like to thank everyone who made a contribution to my thesis. Also to all the people I forgot or do not call by name below. First of all I would like to thank my both VKI promoters. Guillermo Paniagua and Victor Fernández Villacé for their guidance, theoretical support and the help finding the exact information I was searching for. Also thanks to my KHBO promoter, Wim Vanparys who also gave me support, in addition to his clear view on the project and future considerations. Second I would like to say thank you to JeanFrançois Herbiet for his EcosimPro help, in which Victor also made his contribution, and for the information about the conical inlet and its implementation. Without the IT help of Olivier Jadot there would be no EcosimPro at the VKI, on my computer and it definitely would not be accessible at home. Also the people of the VKI library deserve a great thank you for delivering the requested papers as soon as possible which were essential to understand the working principle of the RTA. Next, a thank you to my VKI-colleagues, Piet Van den Ecker, Marylène Andre and Maarten De Moor for the great time and discussions about the occurring problems. Most of the time they helped me, without them knowing it, determining and resolving the problems. Of course to all the others as well, to keep up the spirit in the little room were we spent our time. -
Philippe Rahm
Richardson Forecast Factory, 1922 Factory, Forecast Richardson réservés - droits © Alf Lannerbäck LLee parlementparlement climatique climatique Pavillon de l’Arsenal 24-25.01.20 | Pavillon de l’Arsenal 24-25.01.20De quoi le consensus écologique est-il le nom ? De quoi le consensus écologique est-il est-il le le nom nom? ? VendrediVendredi 24.01 24.01 Samedi 25.01Samedi 25.01 Avec les conférences de du 27.01 au 31.01 -— au au Pavillon Pavillon de del’Arsenal l’Arsenal — au Pavillon- deau Pavillonl’Arsenal de l’Arsenal Alessandro Bava et Rebecca- à l’ENSA-V 13:3013:30 - - Accueil Accueil 14:30 - Accueil14:30 - Accueil Sharp, Holly Jean Buck, NathalieWorkshop Master 1 14:0014:00 - - Introduction Introduction par les organisateurs15:00 - Introduction15:00 - Introduction par lesDe organisateurs Noblet-Ducoudré, Platon 14:1514:15 - - Ouverture Ouverture : Nathaliepar Nathalie de Noblet-Ducoudré de 15:00 - Troisième 15:20 table- Léa rondeMosconi Issaias, Samaneh Moafi, JasonSamedi 01.02 15:30Noblet-Ducoudré - Table ronde 1: Grégory Quenet, 17:00 - Film15:50 «Human - Samaneh mask» Moafide W. Moore, Léa Mosconi, Grégory- à l’ENSA-V Philippe15:30 - Rahm,Première Roger table Tudo ronde Pierre Huyghe16:20 - Alessandro Bava &Quenet, Rebecca Philippe Sharp Rahm, IvonneExposition dans le cadre de la journée 17h3018:30 -- TableSeconde ronde table 2: Ivonne ronde Santoyo-Orozco,19:00 - Cocktail16:50 - Discussion de clôtureSantoyo-Orozco, avec l’ensemble Roger Tudó...des Portes Un Ouvertes Holly Jean Buck (online), Jason Moore (online), des intervenants événement organisé par Nicolas Platondu 27.01 Issaias au 31.01 Samedi 01.0218:00 - Cocktail Dorval-Bory, Emeric Lambert et — à l’ENSA-V — à l’ENSA-V Jeremy Lecomte dans le cadre ConversationsWorkshop Master modérées 1 par Jeremy LecomteExposition dans le cadre de de la semaine blanche 2020 de la journée portes ouvertes l’ENSA-V.