MAE 1202: AEROSPACE PRACTICUM Lecture 1: Introduction and Course Overview January 7, 2013 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk LECTURE OUTLINE • Syllabus • Course Structure • Topics Covered • Advice for MAE 1202 and Florida Tech • Summary Course Website http://my.fit.edu/~dkirk/1202/index.html MAE 1202: COURSE STRCUTURE • Monday lecture to introduce elementary design concepts related to: 1. Aerodynamics (Chapters 4 and 5) 2. Aircraft performance (Chapter 6) 3. Aerospace structures (Chapter 10) 4. Propulsion: Air-breathing, rocket and spacecraft (Chapter 9) • Bi-weekly laboratory sessions – Tuesday and Thursday – or – Wednesday and Friday, Room 228/229 EC – Attendance is taken at every session – free 5% of your grade • Introduce computational engineering tools – MS Word, MS Excel, MATLAB, and Computer Aided Design (CAD) Software • Introduction to machine shop • Introduction and tour of research laboratories – Wind tunnel, shock tunnel, structures, heat transfer, etc. • Team project to design, analyze, and build aerospace device – 5-8 students per team – Design competition held during final week of class READING AND HOMEWORK ASSIGNMENTS • Reading Assignment: – For January 14, 2013 lecture: Chapter 4, Sections 4.1 - 4.14 • Lecture-Based Homework Assignment: – Problems: None • Due Date: • Turn in hard copy of homework – Review and be familiar with textbook examples in Chapter 4 – Note: Answers to all homework problems are provided – grading is dependent on your approach and procedure to arrive at a solution – Comment on your answers – just a phrase or two • Laboratory Homework Assignment #1: – Due Date: Friday, January 18, 2013 by 11 AM – Details in Thurs./Fri. laboratory session LABORATORY INSTRUCTORS Section Date and Time Room 1 Tues. and Thurs.: 9:30-10:45 AM 229 EC 2 Tues. and Thurs.: 2:00-3:15 PM 229 EC 3 Wed. and Fri.: 8:30-9:45 AM 229 EC 4 Tues. and Thurs.: 11:00-12:15 AM 229 EC 5 Tues. and Thurs.: 8:00-9:15 AM 228 EC 6 Tues. and Thurs.: 8:00-9:15 AM 229 EC Teaching Assistant Joel Faure jfaure@my.fit.edu Joel Faure Darren Levine dlevine2008@my.fit.edu Darren Levine Sunil Chintalapati chintals@fit.edu Sunil Chintalapati • GSA = Graduate Student Assistant – Paid to go to grad school – Work on cutting edge research – Also teach and continue to take classes • Are available to help with any homework or laboratory project • Make sure they know who you are – become their friends – Learn about their research – Learn from their successes and mistakes as undergraduates – Ask them questions about how to be successful at Florida Tech LECTURE TOPICS OVERVIEW Aerodynamics Vehicle Performance Propulsion Structures PRICE OF OIL vs. AIRLINE STOCK PRICE Crude Oil (OIS) American Airlines (AMR, AAMRQ) FUEL COST DRIVERS • Fuel now largest component of operating costs • Carriers turning to fuel-saving measures that once seemed hardly worthwhile – Upswept wingtips to increase range and improve aerodynamics – Taxi to and from runway on one engine to save fuel – Does it make sense to actually fly slower? – Do you polish an airplane or paint the airplane? – Airlines have new program to wash their aircraft/engines – Other cost saving measures • 1st and 2nd bag check fee (and many others new fees…) • Remove all pillows from MD-80’s • Think about bankruptcies and mergers over last several years (Delta, American, Continental, United, America West, ATA, etc.) CHEMICAL EMISSIONS AIRCRAFT NOISE AIRCRAFT AND ENGINE NOISE LECTURE TOPICS: AERODYNAMICS • Why are airplanes, wings, rockets, etc. shaped way they are? • What is relevance of their shape? • How do we design such shapes and what is impact of that design? Boeing 777 SR-71 U-2 F-15 HOW DOES AN AIRFOIL GENERATE LIFT? • Lift due to imbalance of pressure distribution over top and bottom surfaces of wing – If pressure on top is lower than pressure on bottom surface, lift is generated – Why is pressure lower on top surface? • We can understand answer from basic physics: – Continuity (Mass Conservation) – Newton’s 2nd law (Euler or Bernoulli Equation) COMMERCIAL AIRCRAFT: BOEING SERIES 707 757 727 767 737 747 • What is same? • What is different? • Why? 777 787 BOEING 747-110 (1973) vs. 747-800 (2009) Airbus Advanced Concept Aircraft 16 http://www.dailymail.co.uk/travel/article-1315836/Boeing-takes-Airbus-invisible-planes-supersonic-scramjet-engines.html EXAMPLE: SLATS AND FLAPS EXAMPLE: SWEPT WINGS • All modern high-speed aircraft have swept wings: WHY? DRONES IN THE NEWS… DO YOU NEED WINGS TO FLY? "At some point I collided with one of the Skyhawks, at first I didn't realize it. I felt a big strike, and I thought we passed through the jet stream of one of the other aircraft. Before I could react, I saw the big fireball created by the explosion of the Skyhawk.” SUPERSONIC FLOW • Can you fly faster than the speed of sound, HOW? • What can happen in supersonic flows? • Supersonic flows (M > 1) are qualitatively and quantitatively different from subsonic flows (M < 1) OTHER APPLICATIONS OF AERODYNAMICS ROCKET VS. AIR-BREATHING PROPULSION • Take mass stored in a vehicle and • Capture mass from environment and set throw it backwards that mass in motion backwards → Use reaction force to propel → Use reaction force to propel vehicle vehicle – Only fuel is carried onboard – All fuel and oxidizer are carried – Oxidizer (air) is ‘harvested’ onboard the vehicle continuously during flight – Rocket and Mission Analysis (MAE: 4262) – Air-Breathing Engines (MAE: 4261) CROSS-SECTIONAL EXAMPLE: GE 90-115B Compressor Nozzle Fan Turbine Inlet Combustor • Why does this engine look the way that it does? • How does this engine push an airplane forward, i.e. how does it generate thrust? • What are major components and design parameters? • http://www.geae.com/education/genx/theatre/genx_theatre_go.html TRENDS TO BIGGER ENGINES 1958: Boeing 707, United States' first commercial jet airliner Similar to PWJT4A: T=17,000 lbf, a ~ 1 1995: Boeing 777, FAA Certified PW4000-112: T=100,000 lbf , a ~ 6 COMMERCIAL VS. MILITARY ENGINES (APPROX. SAME THRUST, APPROX. CORRECT RELATIVE SIZES) GE CFM56 for Boeing 737 T~30,000 lbf, Bypass Ratio, a ~ 5 P&W 119 for F- 22, T~35,000 lbf, Bypass Ratio a ~ 0.3 HOW ARE ROCKET NOZZLES SHAPPED? • ConvergingDiverging shape is ONLY way to accelerate a subsonic flow to super sonic velocities! LECTURE TOPICS: AIRPLANE PERFORMANCE 747 What drove this design? Fuel Cost 787 • • Examine behavior of entire airplane – How fast can this airplane fly (Range)? – How far can this airplane fly on a single tank of fuel (Endurance)? – How long can this airplane stay in the air on a single tank of fuel? – How fast and how high can it climb? – How well can the airplane maneuver? How does the airplane perform? EXAMPLE: VIRGIN ATLANTIC GLOBALFLYER World record for first non-stop solo circumnavigation around the world Wing Span: 114 ft Wing Area: 400 ft2 Length: 44.1 ft Height: 13.3 ft Gross Weight: 22,000 lbs Empty Weight: 3,350 lbs LECTURE TOPICS: AEROSPACE STRUCTURES • Structural analysis plays a key role in aerospace design – Just as important as aerodynamics, propulsion, flight dynamics and control • Vast resources (money, time, etc.) dedicated to reducing weight and cost of aerospace structures • Aerospace structures operate in unique (often very harsh) environments – Rockets: High G-loading and dynamic pressure (yet want lightweight and thin tanks to reduce mass penalty) – Gas turbine engine blades: Operate above the melting temperature of material! Structure must be cooled EXAMPLE: SPACE STATION TRUSS STRUCTURE In a weightless environment load calculations become easier? No. Truss system being built for International Space Station must withstand both loading from launch and unusual forces and environment found on orbit. EXAMPLE: AIRCRAFT WAKE TURBULENCE STRUCTURAL FAILURE EXAMPLE? • Aug. 5 — The Nov. 12 2001 crash of American Airlines Flight 587 was the world's worst single-plane crash in a decade – Airbus: pilot error as one possible cause – AA: Airbus A300-600's composites, the material that makes up the tail, could have been the culprit • In theory, the airplane should be able to withstand a sudden yaw, yet it is well known that severe and dangerous horizontal gust loads can be imposed on vertical stabilizers under some flight conditions. That is why they have computer monitoring of airspeed so as to reduce the limit of rudder movement, on modern airliners: because structural limits of the vertical stabilizer can be exceeded if the rudder throw is too great when accompanied by a severe side loading LABORATORY TOPICS OVERVIEW ENGINEERING TOOLS: MS WORD AND EXCEL • MS Word (1 Lecture) – Introduction of basic and higher order functions • Automatic generation of table of contents, lists of figures and tables • Spell and grammar check • Headers and footnotes • Important to produce professional quality engineering documents • MS Word facilitates document generation, but quality of technical writing is still up to you • MS Excel (1 Lecture) – Introduction to spreadsheet analysis – Introduction of basic and higher order functions • Freezing rows and columns, goal seek, generating plots ENGINEERING TOOLS: MATLAB • Overview of Matlab: 4 Lectures • What is it and what can it do? – Matlab is a mathematical software that can be used to solve a wide range of engineering problems – Write your own programs and utilizes many ‘built-in’ functions • Sum, mean, pi, sin, std, max, factorial, etc. – Very powerful for manipulation of matrices, linear algebra – Data analysis and plotting ENGINEERING TOOLS: CAD • One of most sophisticated and powerful solid modeling packages available • Provide foundation on how to use package over course of ~10 laboratory sessions • • • • Create models of relatively complex parts and assemblies Know how to produce related detailed engineering drawings Understand terminology use in CAD Understand design philosophy and methods embedded in CAD CADPROFESSIONAL EXAMPLES PREVIOUS CAD FIT PROJECTS PREVIOUS CAD FIT PROJECTS EXAMPLES MACHINE SHOP OVERVIEW • Useful throughout time at FIT, especially Junior and Senior Design Projects • Knowledge of how various components are made ↔ design process • Basic Machine Shop Training (6 sessions) – Shop Safety – Drawing and Manufacturing – Precision Instruments – Cutting Tools, Milling Machine, Saws, Welding, Lathe, Hand Tools, etc. Example: Inside Micrometer Example: Outside Micrometer LABORATORIES OVERVIEW • A wind tunnel is a ground-based experimental facility used to produce air flow to study flight of airplanes, missiles, space vehicles, etc. • Many different types of wind tunnels – Subsonic, transonic, supersonic, hypersonic Excellent Wind Tunnel Site: http://vonkarman.stanford.edu/tsd/pbstuff/tunnel/ TEAM PROJECT GOAL: Launch and recover student designed, Built, and tested rockets to a given altitude Excellent preparation for junior and senior design projects and Pioneer Cup Participation FREE ADVICE STATISTICS AND COMMENTS • Aerospace Engineering largest major, in largest department, in largest college at Florida Tech (lots of leverage) • 86 students currently enrolled in 2013 MAE 1202: Aerospace Practicum • 100 students initially enrolled in 2012 MAE 1201: Introduction to Aerospace Engineering – 14 % loss in enrollment – 2010: 93 in Intro, 74 started Practicum (20% loss) – 2007: 105 in Intro, 91 started Practicum (13% loss) • Last year Aerospace Practicum had 72 students • 30% A’s • 45% B’s • 2 F’s THE GOOD ABOUT MAE 1202 • Class is exceptionally difficult to fail – or even get a D – Nonetheless it happens, however never because of academic inability • Doing all homework, participating in team project, attending every lab, and taking every concept quiz will probably get you a B • Team project turns out to be a lot of fun – You will be graded by your teammates for project – Projects are well-funded • Take advantage of office hours and many evening review sessions • Exams follow closely from lecture concepts, homework and text reading – Exams are open book and notes – Exams are rather lengthy and challenging • Foundation for many course at Florida Tech THE BAD ABOUT MAE 1202 • Foundation for many course at Florida Tech • Course is listed as 2 credits – it will feel like 4 – Lots of lecture homework (~8 problems per week) • Lots of new fundamental concepts – Laboratory assignment every week – New engineering tools (MATLAB and Pro|Engineer) to learn – Team project is a lot of work • You probably will like aspects of the course better than others • Your team may work well together or you may not work together • There will undoubtedly be complaining – Complain to me – never to your Teaching Assistants HOWEVER: If you dedicate yourself to doing all this work: You will be extremely prepared for all other aerospace courses at FIT You will be among the most prepared and knowledgeable sophomores OTHER ADVICE • College is 3½ years long, not 4 – When you apply for grad school or a job, your transcript will only cover your first 7 semesters! – Job offers or a grad school plan in place before your last semester is over • The difference between a 3.01 GPA and a 2.98 GPA is much larger than the difference between a 3.2 and 3.5 GPA – 3.01 GPA grad school, completely paid for = yes! – 2.98 GPA grad school = bye bye, good luck not finding a job! • It is almost impossible to dig out of a big GPA hole • Pay attention to 4 credit courses – Big ‘hitters’ in your GPA – Be well rounded, but balanced – we don’t need engineering dorks • Setting a good precedent early is important – without being a suck-up – Good student – As I grade this exam, let me find where to give her points – Bad student – As I grade this exam, let me find where she went wrong COURSE SUMMARY • MAE 1202: Aerospace Practicum offers exciting mix: – Interesting lectures • Aerodynamics, propulsion, flight performance, structures • Content will extend through FIT, grad school, career – Introduction to modern and highly useful engineering tools • MS Word, MS Excel, Matlab, Pro|Engineer Wildfire – Tour of machine shop and research laboratories – Design Project • Opportunity to work in teams on aerospace related project • Apply theoretical results with engineering tools • Design, analyze, and build ONLINE REFERENCES • • • • • • • • • • • http://www.aircraftenginedesign.com/enginepics.html http://www.pratt-whitney.com/ http://www.geae.com/ http://www.geae.com/education/engines101/ http://www.ueet.nasa.gov/StudentSite/engines.html http://www.aeromuseum.org/Education/Lessons/HowPlaneFly/HowPlaneFly.html http://www.nasm.si.edu/exhibitions/gal109/NEWHTF/HTF532.HTM http://www.aircav.com/histturb.html http://inventors.about.com/library/inventors/bljjetenginehistory.htm http://inventors.about.com/library/inventors/blenginegasturbine.htm http://www.gas-turbines.com/primer/primer.htm