Introduction Lecture 1 ME EN 415 Andrew Ning aning@byu.edu - - PowerPoint PPT Presentation
Introduction Lecture 1 ME EN 415 Andrew Ning aning@byu.edu - - PowerPoint PPT Presentation
Introduction Lecture 1 ME EN 415 Andrew Ning aning@byu.edu Syllabus http://flow.byu.edu/me415/ 515 (595R): 510: Compressible 541: Computational Aerodynamics Fluid Flow Fluid Dynamics 415: Flight Vehicle 523: Aircraft 456/602: Design
Syllabus
http://flow.byu.edu/me415/
415: Flight Vehicle Design 515 (595R): Aerodynamics 510: Compressible Fluid Flow 541: Computational Fluid Dynamics 426: Gas Turbine and Jet Engine Design 523: Aircraft Structures 456/602: Composites 431: Control Systems 634: Flight Dynamics and Control 575: Design Optimization ChE 693R: Dynamic Optimization
Grading
Homework 400 Exams 400 Project 150 Quizzes 50 Total 1000
Aircraft Industry
Air travel has proved to be resilient to external shocks
World annual traffic (trillion RPKs)
Oil Crisis Gulf Crisis Oil Crisis Asian Crisis WTC Attack SARS Financial Crisis
x2
since 9/11
+60%
growth over the last 10 years 1 2 3 4 5 6 7 8 1966 1971 1976 1981 1986 1991 1996 2001 2006 2011 2016
Airbus Global Market Forecast 2017
FAA Aerospace Forecast 2017
Air Transportation Economics
source: Javier Irastorza Mediavilla
Air Transportation Safety
Aviation Safety Network
1.5 3 4.5 6 Motorcycles Cars & Trucks Commuter Rail Subways Bus Plane 217 Deaths per billion passenger miles (USA)
Air Transportation Efficiency
$0 $20 $40 $60 $80 $100 $120 $140 2000 2005 2010 2015 2020 2025 2030 2035 $ Per Barrel of Oil
Fiscal Year
U.S. Refiners' Acquistion Cost
Source: IHS Global Insight
% of base (Comet 4)
Year of model introduction 1950 100 90 80 70 60 50 40 30 20 10 1960 1970 1980 1990 2000 2010 49% 82%
Comet 4 707-120 747-100 DC-8-63 747-400 Engine fuel consumption Aircraft fuel burn per seat 777-200 777-200 777-300ER 777-300ER A380 A380 787 787
Fuel efciency gains since the early jet age
Design
The Future of Airplanes The Future of Space Exploration
Main Design Parameters
fmincon
Wingspan Chords Tail Sizing Volume Coefficients C.G. Landing Gear Furnishings Fuselage Wing Tail Engine Structure Battery Battery C.G. + Sizing Lattice (Tornado) Trim (Tornado) Parasitic CD L/D CL & CD at each flight stage Vclimb Vmax Vcruise Define Ultimate Loads Wing Loadings V-n Diagram Range Velocity Climb Time Efficiency 2D/3D View Performance Plots Inequality Constraints Equality Constraints Design Parameters Design Performance Global Assumptions Wing + Tail Sizing Component Masses Drag Polar Velocity Performance V-n Diagram Performance Calculation Aircraft Computation (optimization) xt
Specifications Conceptual Design Preliminary Design Detail Design Flight Tests Operations Growth Versions History & Archive Market/Operations Research
Adapted from a Boeing flow chart