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AAE 490 - AAE 490 - Purdue Study Resources
  • 14 Pages Land Speed Record
    Land Speed Record

    School: Purdue

    Land Speed Record Streamlined Motorcycle Purdue University - School of Aeronautics and Astronautics Past and Current Streamliners Sam Wheeler EZ-Hook 277 mph Purdue University - School of Aeronautics and Astronautics Virtual Edge Goal 90 km in one hour (5

  • 4 Pages progress_report3
    Progress_report3

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 3 Week 3 (02/08/08 02/14/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright J

  • 7 Pages progress_report4
    Progress_report4

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 4 Week 3 (03/07/08 03/20/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright J

  • 7 Pages progress_report5
    Progress_report5

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 5 Week 3 (03/07/08 03/20/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright J

  • 7 Pages progress_report6
    Progress_report6

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 6 Week 3 (03/21/08 03/27/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Sricharan Ayyalasomayajula Jennifer Jackson

  • 6 Pages progress_report7
    Progress_report7

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 7 Week 9 (3/28/08 4/3/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright Jenn

  • 5 Pages progress_report8
    Progress_report8

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 8 Week 10 (4/4/08 4/10/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright Jen

  • 6 Pages progress_report9
    Progress_report9

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 9 Week 11 (4/4/08 4/17/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright Jen

  • 15 Pages progressfeb_28
    Progressfeb_28

    School: Purdue

    AAE 490T/590T AT 490D Tech 581N Design/Build/Test Progress Report On Oblique Wing with Extendable Span Project February 28, 2003 Name Jeff Decker Wade McMillan Doug Mousseau Stephanie Steber Hours worked Signature 1.0 Introduction This week, most of the a

  • 5 Pages progressreport_April11_2003
    Progressreport_April11_2003

    School: Purdue

    . . . . . . AAE . . . 490T/590T AT 490D Tech 581N Design/Build/Test Progress Report on Seraphim Program (VTOL Aircraft) Date April 11th, 2003 Name Hours worked Brent Robbins 20+ Chris Fisher 20+ See-Chen Lee 20+ Signature X X X . . . . . . . . . AAE 490T

  • 8 Pages part_detect_paper
    Part_detect_paper

    School: Purdue

    SSC02-IX-4 Design and Test of a Solid State Charged Particle Detector for Cubesat Michael Dowler, Victor Aguero*, Stephen Sears, Robert Twiggs*, Jim Albers, Kathy Lee, Gordon Maahs Lockheed Martin Space Systems Company, Sunnyvale, CA * Stanford Research I

  • 1 Page quiz1sol
    Quiz1sol

    School: Purdue

  • 2 Pages quiz2sol
    Quiz2sol

    School: Purdue

  • 1 Page quiz3sol
    Quiz3sol

    School: Purdue

  • 1 Page quiz4sol
    Quiz4sol

    School: Purdue

  • 2 Pages quiz5sol
    Quiz5sol

    School: Purdue

  • 3 Pages progress_report2
    Progress_report2

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 2 Week 3 (02/01/08 02/07/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright J

  • 3 Pages progress_report1
    Progress_report1

    School: Purdue

    Demonstration of Flight Characteristics Using a Scaled Aircraft Model AAE 490T/590R Team #4 Progress Report 1 Week 2 (1/24/08 1/31/08) Meeting Times: Tuesday 4:30pm-6:00pm Thursday 10:15am-12:00pm Team Members Tatsuya Kotegawa David Predis John Wright Jen

  • 5 Pages Progress Report - March 29
    Progress Report - March 29

    School: Purdue

    Experimental Assessment of the Aerodynamic Performance of Numerically Optimized Rotor-blade Airfoils David Fanjoy Eddie Prez-Rubert AAE 520 Final Project FS-GA1 Result of a shape design procedure with a Genetic Algorithm Aerodynamic analysis from a pane

  • 2 Pages why-study-viscous-flow
    Why-study-viscous-flow

    School: Purdue

    Why Study Viscous Flow? 1. 2. 3. Skin Friction can be significant to Drag. For slender high L/D vehicles at all speed ranges. Global Hawk to NASP. Boundary-layer Separation is one example of critical viscous/inviscid interactions. Can be a major factor in

  • 22 Pages Large_Metal_Aircraft
    Large_Metal_Aircraft

    School: Purdue

    StructuralHealth MonitoringDemonstrator (SHMD) GroupMembers:JoshuaSiler StasYerusky JoeWelch DavidHarsanyi SethLimp NatashaWall BrianHutto BryanEngle PaulReiber MissionOverview MissionOverview SHMDusage MechanicalEngineeringandAviation Technologycollabo

  • 3 Pages wiltz-in-streamliner
    Wiltz-in-streamliner

    School: Purdue

  • 28 Pages mav_report-fall99
    Mav_report-fall99

    School: Purdue

    Design, Construction, and Testing of a Micro Air Vehicle Prototype Thra Bundechanan Patrick Dempsey Paul Klusman Thomas Schmidt-Lange (Final report assembled and edited by T. Schmidt-Lange with assistance from P. Dempsey and P. Klusman.) AAE490 Purdue Uni

  • 17 Pages MBagg AAE415
    MBagg AAE415

    School: Purdue

    WingStrake WingStrake MatthewBagg AAE415 Overview Overview Introduction Purpose Procedure Results Conclusions Introduction Introduction WhatareThey HowStrakesWork CreateVortex DelaysSeparation PastResearch SupersonicFlight HighAngleofAttack ControlSurface

  • 17 Pages Micro Air Vehicles
    Micro Air Vehicles

    School: Purdue

    MicroAirVehicles MicroAirVehicles JoshBock EricEagon BrianEnlow JohnMcKinnis ColleenRainbolt AAE490TSpiral1Presentation,February7,2004 Background Background WhatisaMicroAirVehicle (MAV)? Fullyfunctionalplane <6inchdimension Aerialrobot WhatareMAVsuse

  • 6 Pages Micro Air Vehicles(spring 03)
    Micro Air Vehicles(spring 03)

    School: Purdue

    MicroAirVehicles MicroAirVehicles ChrisKrukowski LouHuebsch DanTrigg JonDavid 272003 ProjectGoals ProjectGoals Todesign,buildandflyamicroairvehicle Todevelopaflightcontrolsystemfora MAVthatmakesflyingsimple TobuildaMAVsothatitiscostefficient WhatisaMAV? W

  • 4 Pages naca airfoils
    Naca Airfoils

    School: Purdue

    NACA 0021 2 1.5 1 Cl 0.5 0 - 12 -10 -8 -6 -4 -2 0 2 4 6 8 10 12 -0.5 -1 -1.5 Column C -2 Angle o f a t t a ck () Column D NACA 0021 0.014 0.012 0.01 Cd 0.008 0.006 0.004 0.002 0 -1.5 -1 -0.5 0 Cl 0.5 1 1.5 NACA 0010 2 1.5 1 0.5 Cl 0 - 15 -10 -5 0 5 -0.5 -

  • 49 Pages Oblique_Morph_CDR
    Oblique_Morph_CDR

    School: Purdue

    Obliquing Wing with Extendable Span Critical Design Review AAE 490T/590T AT 490D Tech 581N Design/Build/Test Professor John Sullivan Professor William Watkins Spring 2003 Purdue University School of Aeronautics and Astronautics 1282 Grissom Hall West Lafa

  • 1 Page olivia
    Olivia

    School: Purdue

    AR[old] b=[in] c=[in] S=[in2] 45 18 810 Clalph CL 2.5 3.489 e(oswald eff) CD 0.9695 0.0250 AR[new] b=[in] c=[in] S=[in2] 61 18 882 4.22 e(oswald eff) CD 0.9579 Assume alph= V= 8 deg 200 mph CL CDMin 0.0242 CDMin 4.260 0.5325 0.0214 Decrease 0.0224 11% CL

  • 4 Pages our airplane
    Our Airplane

    School: Purdue

    Power Propeller Eff 1 hp 0.8 Density 0.002378 lb/ft^3 W b=wing span Area c= chord AR 5 lb 4 ft 6 ft^2 1.5 ft 2.666667 Cdo e k 0.01 0.93 0.128351 ft/sec Velocity wing loading lb/ft^2 W/A 0.833333 lb/ft^2 lbf hp q Drag Power Required 1 0.001189 74.96430398

  • 1 Page outboard section
    Outboard Section

    School: Purdue

  • 1 Page power_budget
    Power_budget

    School: Purdue

    Power Budget Total Power Calculated Estimation Our System Budgeted Estimate Subsystem Percentage Allocated Standby Peak Thermal 7.65% 0.14 C&DH 7.65% 0.14 Comm. 10.93% 0.2 Magnetometer 16.39% 0.3 Other 0.00% Science - Camera 30.05% 0.55 Science - Detector

  • 20 Pages PrelimDesignNEPmission
    PrelimDesignNEPmission

    School: Purdue

    Preliminary Design of Nuclear Electric Propulsion Missions to the Outer Planets Chit Hong Yam,* T. Troy McConaghy, K. Joseph Chen* and James M. Longuski School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47907-2023 Nuclear

  • 7 Pages presentation
    Presentation

    School: Purdue

    The Seraphim Program The Seraphim Part I AdvancedVTOLAircraftConcept BrentRobbins ChristopherFisher DanielChakraborty SeeChenLee Project Proposal Project PresentationOverview ProjectObjective BaselineDesign DesignStrategies ConstructionStrategies ProjectT

  • 1 Page quiz6sol
    Quiz6sol

    School: Purdue

  • 32 Pages BOS_Final_Report
    BOS_Final_Report

    School: Purdue

    Background Oriented Schlieren Purdue University AAE 490R/590R 2 May 2008 Landon Baur John Tapee Table of Contents 1 Introduction. 2 1.1 Project Goal . 2 1.2 Background . 2 1.3 Reasons for Using Background Oriented Schlieren . 4 2 Apparatus . 5 2.1 Schemat

  • 6 Pages exam1bsol
    Exam1bsol

    School: Purdue

  • 4 Pages hw8sol
    Hw8sol

    School: Purdue

  • 1 Page hw9
    Hw9

    School: Purdue

    EE610 HW#9 - Due November 15, 2011 1) problems 5.18, 5.19, 5.20 (Assume the machine is 3-Phase), 5.22, 5.24, 5.25, 5.26 in Krause, Wasynczuk, and Sudhoff. 2) Starting with the steady state equations in the rotor frame of reference. Derive the phasor equiv

  • 11 Pages hw9sol
    Hw9sol

    School: Purdue

  • 2 Pages hw9solcor
    Hw9solcor

    School: Purdue

  • 2 Pages hw10
    Hw10

    School: Purdue

    ECE 610 -HW#10, Due December 1, 2011 1) For the induction machine shown in Figure 4.2-1. Derive expressions for MMF ar , MMF br , 2 and MMF cr . If i ar = cos ( ( e r ) t ) , i br = cos ( e r ) t - , 3 2 i cr = cos ( e r ) t + - . Show the speed and direc

  • 18 Pages hw10sol
    Hw10sol

    School: Purdue

  • 25 Pages hw11
    Hw11

    School: Purdue

    EE610 HW#11 2011 - Not to turn in 1) Using the voltage waveform shown in Figure 13.3-2, use a Fourier Series to derive the fundamental component of the phase voltage v as . 2) Given a single-phase H-bridge inverter. The output voltage is shown. The output

  • 12 Pages hw11sol
    Hw11sol

    School: Purdue

  • 22 Pages surfcam-lecture-old
    Surfcam-lecture-old

    School: Purdue

    Introduction to SurfCam And CNC Machining John Sullivan Purdue University 494-3344 sulivan@ecn.purdue.edu http:/roger.ecn.purdue.edu/~490t/ Purdue University - School of Aeronautics and Astronautics Design/Build/Test Environment Design Computers Software

  • 13 Pages lecture1
    Lecture1

    School: Purdue

  • 20 Pages Team #2_Storm Glider_Critical Design Review_Supporting Document
    Team #2_Storm Glider_Critical Design Review_Supporting Document

    School: Purdue

    AAE 490/590t/CGT 423 Storm Glider Design Review Document March 10, 2004 Steven Blaske, Matthew Branson, Heather Dunn, Leslie Martin, Nicholas Nugent, Enrique Portillo Carrie Spear OBJECTIVE / MISSION Project Motivation One of the most common ways to colle

  • 19 Pages DesignReview3_9_01
    DesignReview3_9_01

    School: Purdue

    HYPERIONDesignReview AAE 490T/590T March 9th, 2001 PRESENTED BY: John Castro Loren Garrison Chris Peters Jeff Rodrian Thomas Schmidt-Lange Outline Historical Database Parameter Selection Weight Determination Fixed Weights Weight Estimation Process Opti

  • 10 Pages Team9_motorcycle_DesignReview_r2
    Team9_motorcycle_DesignReview_r2

    School: Purdue

    Streamlined Motorcycle Documentation AAE 490T Design Build Test Team 9 Yohei Sugiyama John Meyers Robert Jacobs Matt Capria David Earle Matt Koehl March 10, 2004 Mission Statement Our mission is to produce a fin for the streamlined motorcycle that will pr

  • 10 Pages Lit_Review_Pres_1-17
    Lit_Review_Pres_1-17

    School: Purdue

    Background Oriented Schlieren Landon Baur John Tapee Classical Schlieren Setup Index of refraction is proportional to density Sensitive to density gradient in transparent medium Works best in 2D environment where collimated light rays are perpendicular to

  • 2 Pages SYLLABUS
    SYLLABUS

    School: Purdue

    Last Revised: August 9, 2010 Course Outline A&AE 613 Viscous Flow Theory Prof. S. Schneider, Fall 2010 Prof. Steve Schneider Lab Oce: 13C Aero. Sci. Lab., x43343 Email: steves@purdue.edu Campus Oce: ARMS 3213, x45254 I spend most of my time at my lab oce.

  • 13 Pages hw7sol
    Hw7sol

    School: Purdue

  • 17 Pages hw6sol
    Hw6sol

    School: Purdue

  • 16 Pages hw5sol
    Hw5sol

    School: Purdue

  • 4 Pages exam1sol
    Exam1sol

    School: Purdue

  • 5 Pages exam2bsol
    Exam2bsol

    School: Purdue

  • 6 Pages exam2sol2
    Exam2sol2

    School: Purdue

  • 6 Pages exam11sol
    Exam11sol

    School: Purdue

  • 195 Pages Final Report
    Final Report

    School: Purdue

    AAE 490 Grand Prix Kart Design Capstone Design Class Purdue University Spring 2006 Ian Thomson, Team Leader Clayton Smith, Driver Michael Nash Joseph Trager Table of Contents 1 INTRO.5 1.A PROJECT CONCEPT.5 1.B RACE BACKGROUND. 5 1.C TEAM SMITH BACKGROUND

  • 10 Pages finalpresentation-LDB
    Finalpresentation-LDB

    School: Purdue

    Outline Motivation Theory ProjectAssembly Testing Conclusion Motivation Cost Analysis Less drag = less fuel Less drag = greater payload for same fuel Less drag = greater distance Theory Laminar Flow Strattford Pressure Recovery region Streamlined Body

  • 28 Pages PIV_final
    PIV_final

    School: Purdue

    KaraAkgulian,BrianErson,NixonLange JaredScheid,SolomonWesterman www.purduepiv.info WhatdoesPIVdo? Howdoesitwork? Wheredidwestart? Wherewearenow Conclusion Opticaltooltoanalyzeflows Createsavectorfieldtoillustratethedirectionand magnitudeoftheflow Ou

  • 8 Pages Progress Report Example1
    Progress Report Example1

    School: Purdue

    Progress Report #2 Purdue University Mars Airfoil Research David N. Loffing July 13, 2001 Aerospace Sciences Laboratory Introduction: The purpose of this research project is to investigate the phenomena associated with low-Reynolds number aerodynamics. Tw

  • 5 Pages Progress Report Example2
    Progress Report Example2

    School: Purdue

    Progress Report Fall 2001 Week #5 Eppler 387 Testing David N. Loffing September 15, 2001 Introduction: Preliminary testing of the Eppler 387 last week recorded higher than expected values for drag, compared to data collected by Selig and Eppler.1,2 Change

  • 1 Page hw1
    Hw1

    School: Purdue

    ECE 610 -HW#1, Due September 1, 2011 1. A general expression for the energy in a magnetic system (volumetric) is J m H = H dB - . 3 m a) Derive an expression for the total energy in a volume assuming the material is isotropic and that B = H . Express the

  • 9 Pages hw1sol
    Hw1sol

    School: Purdue

  • 1 Page hw2cor
    Hw2cor

    School: Purdue

  • 7 Pages hw2sol
    Hw2sol

    School: Purdue

  • 5 Pages hw3sol
    Hw3sol

    School: Purdue

  • 10 Pages hw4sol
    Hw4sol

    School: Purdue

  • 1 Page syllabusm
    Syllabusm

    School: Purdue

    ECE633 Modeling and Simulation of Power System Components Objective: To acquaint the graduate student with the analysis and simulation techniques of power system components. Description: This course is recommended for those interested in learning to use c

  • 38 Pages VISTA-Software-Enabled-Control-Overview
    VISTA-Software-Enabled-Control-Overview

    School: Purdue

    VISTA a 21st Century Testbed Click to edit Master text styles Second Level A FT ES T P I L SC OT HO L O Software Enabled Control Principle Investigators Meeting November 13-15, 2001 Major Andrew Rocket Thurling USAF Test Pilot School U S

  • 8 Pages AIAA-3650-983
    AIAA-3650-983

    School: Purdue

    JOURNAL OF SPACECRAFT AND ROCKETS Vol. 37, No. 6, November December 2000 Trajectories to Jupiter via Gravity Assists from Venus, Earth, and Mars Anastassios E. Petropoulos, James M. Longuski, and Eugene P. Bon glio Purdue University, West Lafayette, India

  • 1 Page rib
    Rib

    School: Purdue

  • 1 Page rotation part
    Rotation Part

    School: Purdue

  • 10 Pages AIAA-13095-511
    AIAA-13095-511

    School: Purdue

    JOURNAL OF SPACECRAFT AND ROCKETS Vol. 41, No. 5, SeptemberOctober 2004 Shape-Based Algorithm for Automated Design of Low-Thrust, Gravity-Assist Trajectories Anastassios E. Petropoulos and James M. Longuski Purdue University, West Lafayette, Indiana 47907

  • 1 Page Safety
    Safety

    School: Purdue

    Safety Procedures for CNC Machinery Revised 1-25-00 1. The CNC machines are not to be operated by any individual without proper training and knowledge of either the computer program that runs the router, or the router itself. 2. Safety glasses, available

  • 4 Pages airfoils
    Airfoils

    School: Purdue

    CL vs. Alpha 3 2.5 2 1.5 CL 1 0.5 0 - 15 -10 -5 0 5 -0.5 -1 -1.5 Alpha (deg) 10 15 Column B Column E Column H Column K Column N Column Q Column B Column E Column H Column K Column N Column Q Column B Column E Column H Column K Column N Column Q Column B C

  • 1 Page Schedule of Events
    Schedule Of Events

    School: Purdue

    Team 8 Morphing Aircraft Schedule of Events I. II. III. IV. Due this Friday a. CGT Majors i. PDM ii. Cost Analysis iii. Catia model and animation for telescoping wings iv. Personal powerpoints b. Engineers i. Layout semester schedule ii. Constraint and mi

  • 28 Pages AT91EB40 Evaluation Board
    AT91EB40 Evaluation Board

    School: Purdue

    AT91EB40 Evaluation Board . User Guide Table of Contents Section 1 Overview. 1-1 1.1 1.2 1.3 Scope.1-1 Deliverables .1-1 The AT91EB40 Evaluation Board .1-1 Section 2 Setting Up the AT91EB40 Evaluation Board . 2-1 2.1 2.2 2.3 2.4 2.5 2.6 2.7 Electrostatic

  • 6 Pages Sduct_UAV
    Sduct_UAV

    School: Purdue

    Development of a Modular Inlet/Engine Section for Unmanned Aerial Vehicle Integration AAE 590T February 7, 2003 Ben Stein Objectives: Design and Fabricate Stealthy, Delta Wing Unmanned Aerial Vehicle (UAV) Complete with a Modular Inlet/Engine Section (MI

  • 20 Pages AT91R40807 Electrical Characteristics
    AT91R40807 Electrical Characteristics

    School: Purdue

    Features Incorporates the ARM7TDMI ARM Thumb Processor Core High-performance 32-bit RISC Architecture High-density 16-bit Instruction Set Leader in MIPS/Watt Embedded ICE (In-Circuit Emulation) 136K Bytes of On-chip SRAM 32-bit Data Bus Single-cloc

  • 19 Pages shew-wyman
    Shew-wyman

    School: Purdue

    AAE 490T: Race Car Front Wing Design J T Wyman Leah E A M John Shew 3 Leah Wyman First Spiral: Feb. 7, 2004 Overview Summary of Spiral One Background Design Build Test Projected Development Spiral One Spiral One Use of pre-existing wing Analysis o

  • 1 Page autogyro
    Autogyro

    School: Purdue

    AutogyroAdvantagesAble to fly slowly. Possibly easier to launch. DisadvantagesMore complex than a fixed wing. Must have a disk loading of <8oz/sqft Disk b Disk S W W/S Vcruise CL Initial 13.5 1sqft 6oz 6oz/sqft 22ft/s .671 Final 6 .2sqft 1.5oz 7.6oz/sqft

  • 20 Pages Smith_K
    Smith_K

    School: Purdue

    Kyle Smith AAE 415 Fall 2003 Glider A little Background Power Necessary? 1486 Leonardo da Vinci 1799 - Sir George Cayley 1855 Captain Le Bris Leonardo da Vinci Sir George Cayley Otto Lilienthal Learned from birds Believed that a propulsion device wa

  • 7 Pages AV_Sharrk-Presentation
    AV_Sharrk-Presentation

    School: Purdue

    Powered Trike Sandeep Allakki Scott Bird Vicki Hoyle Rebecca Karnes Brandon Owen Rory Toombs Andy Wiratama January 15, 2012 AV Sharrks AAE 490T/590T Spring 1 Objectives Design and prepare blue-prints for a full-scale powered trike Shrink the design for an

  • 1 Page spar
    Spar

    School: Purdue

  • 19 Pages aae490t_pres1
    Aae490t_pres1

    School: Purdue

    Mission Design and build 2 Micro-Air Vehicle for endurance of 1 hour. Either ICE or electric power propellers will be used. Preliminary Design Specifications Take-off weight - 5oz. Cruise velocity - 25 mph. 6 by 6. S5010 airfoil section will be used for

  • 11 Pages reno2000-0525b
    Reno2000-0525b

    School: Purdue

    AIAA 2000 - 0525 A Design/Build/Test Environment for Aerospace Education John P. Sullivan School of Aeronautics and Astronautics and William A. Watkins School of Aviation Technology Purdue University West Lafayette, IN 38th Aerospace Sciences Meeting and

  • 4 Pages a225
    A225

    School: Purdue

    R AMP A225 TEK ULTRA LOW NOISE: <280 electrons RMS Model A225 is a high performance thin film hybrid charge sensitive preamplifier and shaping amplifier developed especially for high resolution systems employing solid state detectors, proportional counter

  • 849 Pages mst1797
    Mst1797

    School: Purdue

    NOTICE OF REINSTATEMENT INCHPOUND MIL-STD-1797A NOTICE 3 24 August 2004 SUPERSEDING NOTICE 2 19 December 1997 DEPARTMENT OF DEFENSE INTERFACE STANDARD FLYING QUALITIES OF PILOTED AIRCRAFT MIL-STD-1797A, dated 30 January 1990, is hereby reinstated

  • 72 Pages stc_application_guide
    Stc_application_guide

    School: Purdue

    AC 2140 APPLICATION GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE May 6, 1998 U.S. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Washington, DC TITLE 14 OF THE CODE OF FEDERAL REGULATIONS (14 CFR) GUIDANCE MATERIAL Subject: A

  • 6 Pages GPS PEC Method
    GPS PEC Method

    School: Purdue

    USING GPS TO DETERMINE PITOT-STATIC ERRORS Gregory Lewis National Test Pilot School Mojave, CA 14 August 2003 Introduction This flight test technique (FTT) is another way to do the traditional ground course FTT for pitotstatics testing found in any

  • 224 Pages signal
    Signal

    School: Purdue

    E 7 00 FCDBA@98564321) (&% "! ' $ # @ @ @ @ @ @ @ @ @ @ @ @ @ A f@fff@ff@fff@eff@ff@fff@ff@fef@ff@ffff@ff@fefrdRcSbqdpbaRi!h @Qn i T @ % f@fff@ff@fff@eff@ff@fff@ff@fef@ff@ffff@ff@fefcdHQQ B9@

  • 4 Pages HOQ examples
    HOQ Examples

    School: Purdue

    QFD Example (modified from Chapter 6 of David Ullman's book, Mechanical Design Process, 2003) Engine Efficiency Battery Cell Power Engine Weight Overall Mass (inclue engine) Maximum Wing Span Aspect Ratio Cabin area Aerodynamic Body Composite applications

  • 4 Pages propellers
    Propellers

    School: Purdue

    Propellers v velocity m/s D diameter m n revolutions per second 1/s density of air kg/m P power W T thrust N http:/www.mh-aerotools.de/airfoils/propuls3.htm Propeller Charts Thrust Coefficient Power Coefficient Matching the Propeller and the Engine What

  • 3 Pages PurchasingMaterials and supplies
    PurchasingMaterials And Supplies

    School: Purdue

    Purchasing Materials and Supplies E-mail a purchase request to sulivan@purdue.edu I will approve and forward to Joan Jackson An example of a purchase request is given below Most purchases should be made through this process. We can get supplies from McMas

  • 85 Pages Purdue_CubeSat_PDR_Presentation
    Purdue_CubeSat_PDR_Presentation

    School: Purdue

    A&AE490Satellite PurdueCubeSat PreliminaryDesignReview December8,2004 PreliminaryDesignReview 8December2004 ProjectEngineerGeorgePollock FacultyAdvisorProf.DavidFilmer PreliminaryDesignReview 8December2004 PreliminaryDesignReview 8December2004 PolyPicosat

  • 6 Pages RakedProposal
    RakedProposal

    School: Purdue

    Performance of Raked Performance Tips During Stall Conditions Conditions Matt Bagg Jeff Komives School of Aeronautics and Astronautics Overview Overview Description Highly Swept Tip Capture Tip Capture Vorticies Vorticies Application Boeing 767-400ER

  • 1 Page 3view
    3view

    School: Purdue

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