Single Line Tethered Glider
|
|
- Marianna Caldwell
- 5 years ago
- Views:
Transcription
1 Single Line Tethered Glider Sub-System Level Design Review Team P14462 Kyle Ball Matthew Douglas William Charlock Jon Erbelding Paul Grossi Sajid Subhani
2 Team Introduction Team Member Major Sajid Subhani Paul Grossi Matt Douglas Jon Erbelding Kyle Ball Bill Charlock Industrial Engineer - Team Lead Mechanical Engineer Mechanical Engineer Mechanical Engineer Mechanical Engineer Mechanical Engineer
3 Agenda Project Description Review Engineering Requirements Review Top 3 Concepts from Last Review Concept Feasibility Glider Analysis and Feasibility Base Station Analysis and Feasibility Project Planning Work Breakdown Structure
4 Project Description Review Goal: Design, build, and test a tethered, small-scale, human-controlled glider. Glider Critical Project Objectives: Maintain maximum tension on the tether Sustaining horizontal and vertical flight paths Measure and record tether tension and position Understand the influential parameters for sustained, tethered, unpowered flight Tether Base Station Operator w/ controller
5 Engineering Requirements Metric No. Metric Marginal Value Ideal Value Units 1 Wingspan <=2 <1 m 3 System Cost <500 $ 4 Length of Looping Flight >2 >=3 min 5 Resolution of Tension Data <=0.1 <=0.01 N 6 Resolution of Angular Position Data <=0.5 <=0.1 deg 7 Typical Repair Time 5 3 min 8 Data Sampling Rate >=100 >=500 Hz 9 Minimal Operational Wind 5 Speed at Ground Level 2.5 m/s Maximum Operational 10 Wind Speed at Ground 5 10 m/s Level 11 Safe for User and Observer Yes Yes Binary 12 Number of Looping Trials >=25 Demonstrated >=30 Integer 13 Training Time (1st Time) <30 <20 min 14 Number of Left Right Horizontal Trials >=25 >=30 Integer 15 Tether length >=15 >=30 m 16 Glider Orientation Knowledge Bridle angle Bridle, yaw, attack, & roll angles deg Yellow: Major design Biege: DAQ Grey: Test flight White: System environment
6 Review of Top 3 System Concepts 3 Single Axis Load Cell IMU with Single Axis Load Cell 2 Potentiometers with Single Axis Load Cell
7 Glider Analysis
8 Choosing the Glider Bixler v1.1 EPO Foam Wing span: 1.4 [m] Chord length: 0.2 [m] Mass: 0.65 [kg] Middle mounted propeller Only EPO Foam $120 Phoenix 2000 EPO Foam Wing span: 2 [m] Chord length: 0.3 [m] Mass: 0.98 [kg] Front mounted propeller Reinforced $150
9 Price Sheet for Glider
10 Choosing the Glider The smaller Bixler glider creates less tension for a larger operating range Able to operate with an affordable load cell
11 Flight Orientation
12 Flight Orientation
13 Flight Analysis Wind Speed: ~ 11 mph
14 Flight Analysis Wind Speed: ~ 22 mph
15 Flight Analysis Wind Speed: ~ 44 mph
16 Qualitative DOE Tension must be less than 5000 [N] (1100 lbs) Slower wind speed: lower tension Larger flight path radius: lower tension Beta angle peaks: ~ Tension peaks: ~ 20 [m] tether length
17 Quantitative DOE Choosing flight configuration Decision variables Beta angle Tether length Flight path radius Constraints Maximum allowable tension Observed wind speed
18 Bridle and Tether Setup Use a tension of 3000 lbs as an overestimate. Maximum allowable stress for Bixler glider: 30 MPa Bridle attached at two points on the fuselage causes structural failure at the wing root with 180 MPa
19 Proposed Tether and Bridle Design
20 Ideal Bridle Location Analysis Optimum tether location: 0.51 m from root. Optimum tether angle: 54 deg from airplane
21 Wing Stress Analysis
22 Wing Stress Analysis Maximum stress: 15 MPa
23 Fuselage Stress Analysis
24 Tether and Bridle Configuration
25 Base Station Analysis and Feasibility
26 Concept 1 2 Potentiometers and Single-Axis Load Cell
27 Vertical Rotation
28 Engineering Spec Considerations Metric No. Metric Marginal Value Ideal Value Units Resolution of Angular 6 <=0.5 <=0.1 degree Position Data δβ = δθ + δγ = 0.5 deg δγ = 0.5 δθ = cos 1 r + Lcos(δφ) L 2 + r 2 + 2rLcos(δφ) From application of Law of Cosines Solve for maximum allowable δφ such that the resolution requirement is met, and load cell begins to move
29 Static Analysis M o = Trsin δφ W LC dcos θ b M pot M bear = 0 T = M pot + M bear + W LC dcos(θ b ) rsin(δφ)
30 Dynamic Analysis M o = Trsin δφ W LC dcos θ M pot M bear = I LC α T = I LCα b + M pot + M bear + W LC dcos(θ b ) rsin(δφ) α b = dω b dt where ω b = ω prcos θ p L + r where θ p = ω p t
31 Horizontal Rotation
32 Static Analysis M o = Trcos(θ b )sin δλ M pot M bear = 0 T = M pot + M bear rcos(θ b )sin(δλ)
33 Dynamic Analysis M o = Trcos(θ b )sin δλ M pot M bear = I LC α b T = I LCα b + M pot + M bear rcos(θ b )sin(δλ) α b = dω b dt where ω b = ω prsin θ p L + r where θ p = ω p t
34 Concept 2 3 Single-Axis Load Cells
35 CAD Model Created 3-D model of the system in SolidWorks Works well when the ball joints are kept in tension as seen in Fig 1. Ball joints fail when they are put into compression as seen in Fig 2. 10/24/2013 Fig. 1 Subsystem Level Design Review Fig. 2 P14462
36 Base Station Cost Feasibility
37 Base Station Equipment Phidgets 3140_0 S Type Load Cell Bourns 3540S-1-103L Potentiometer
38 Initial Base Station Budget Comparison P14462 Purchase List for 3 Load Cell Base Station Part Description Unit Price Qty Individual Total Phidgets 3140_0 - S Type Load Cell Ball End Joint Rod Shipping 0.00 Total Order Price P14462 Purchase List for Potentiometer Base Station Part Description Unit Price Qty Individual Total Phidgets 3140_0 - S Type Load Cell Bourns 3540S-1-103L Potentiometer Miniature Aluminum Base-Mounted Stainless Steel Ball Bearings ABEC Flanged Open 1/2 Inch Ball and Roller Bearing Shipping 0.00 Total Order Price
39 Project Planning Phase 1 Team Organization Problem Definition and comprehension Research complimentary projects Week 3 Presentation preparation Phase 2 Update critical needs on EDGE website Acquire Glider Flight Skills Functional Decomposition Benchmarking base stations Benchmarking marketable Gliders Determine PUGH Diagram Critical eng. theory ID and comprehension Week 6 Presentation preparation Phase 3 Price compare bought gliders/order glider Theoretical flight simulation development Use simulation to calculate feasible tension values Develop preliminary base station sketches and CAD models Preliminary base station calculations for feasibility Understand components of DAQ Identify critical components of DOE Week 9 Presentation preparation Phase 4 Budget approval Finalize base station calculations Fly glider and understand effects of tether Develop implementation of tether/bridal Investigate glider reinforcement options (Carbon fiber) Refine simulation to aid DOE Create algorithm to meet DOE needs Determine specific sensors and building materials Begin to develop/modify LabVIEW code for DAQ Week 12 Presentation preparation Phase 5 Order Materials Week 16 Presentation Gate Review - "Green Light" Week 1 Week 2 Week 3 Week 4 Week 5 Week 6 Week 7 Week 8 Week 9 Week 10 Week 11 Week 12 Week 13 Week 14 Week 15 Week Aug 2-Sep 9-Sep 16-Sep 23-Sep 30-Sep 7-Oct 14-Oct 21-Oct 28-Oct 4-Nov 11-Nov 18-Nov 25-Nov 2-Dec 9-Dec Legend Complete WIP Incomplete
40 Project Planning Phase 3 Price compare bought gliders/order glider Theoretical flight simulation development Use simulation to calculate feasible tension values Develop preliminary base station sketches and CAD models Preliminary base station calculations for feasibility Understand components of DAQ Identify critical components of DOE Week 9 Presentation preparation Phase 4 Budget approval Finalize base station calculations Fly glider and understand effects of tether Develop implementation of tether/bridal Investigate glider reinforcement options (Carbon fiber) Refine simulation to aid DOE Create algorithm to meet DOE needs Determine specific sensors and building materials Begin to develop/modify LabVIEW code for DAQ Week 12 Presentation preparation Week 7 Week 8 Week 9 Week 10 Week 11 Week 12 7-Oct 14-Oct 21-Oct 28-Oct 4-Nov 11-Nov
41 Incomplete Tasks from Phase 3 Control and stability calculations DAQ system development (setup, code) Sensors analysis (calibration, implementation)
42 Work Breakdown Structure (10-12) Paul: Tether and glider reinforcement and DOE Jon: Finalize base station calculations, sensors and build materials Kyle: Finalize base station calculations, sensors and build materials Matt: Tether and glider reinforcement and DOE Saj: Continue to develop DOE, create DOE algorithm, team management Bill: Purchase glider, develop/modify LabVIEW for DAQ, sensors and build materials
43 Questions?
Detailed Design Review
Detailed Design Review Tethered Glider P14462 Outline Engineering Requirements Glider Status Tether Design Base Station Design DAQ System Bill of Materials DOE ANOVA Analysis Test Plan MSD II Plan Work
More informationP14462 Tethered Glider for High Altitude Wind Energy
P14462 Tethered Glider for High Altitude Wind Energy Sajid Subhani Industrial Engineer Matthew Douglas Paul Grossi Kyle Ball William Charlock Jonathan Erbelding 1 Abstract Current wind turbines are limited
More informationUniversity of Colorado, Colorado Springs Mechanical & Aerospace Engineering Department. MAE 4415/5415 Project #1 Glider Design. Due: March 11, 2008
University of Colorado, Colorado Springs Mechanical & Aerospace Engineering Department MAE 4415/5415 Project #1 Glider Design Due: March 11, 2008 MATERIALS Each student glider must be able to be made from
More informationTime Benefits of Free-Flight for a Commercial Aircraft
Time Benefits of Free-Flight for a Commercial Aircraft James A. McDonald and Yiyuan Zhao University of Minnesota, Minneapolis, Minnesota 55455 Introduction The nationwide increase in air traffic has severely
More informationXcalibur. b. Where are the riders torsos nearly vertical with heads down? c. Where are the riders torsos nearly horizontal relative to the ground?
QUALITATIVE QUESTIONS: 1. Watch the ride to see how the orientation of the riders changes. Use the pictures on this page to help you name and describe the positions of riders oriented in the following
More informationRUAT Junior Glider Design Competition Version 1.5
RUAT Junior Glider Design Competition Version 1.5 Version Log Version Date Changes 1.4 Jan 14 1 st Public Version 1.5 Jan 16 Clarified Launch is from spring NOT winch Extended Intent to Compete Deadline
More informationEffect of Support Conditions on Static Behavior of 1400m main span and 700m side span Cable-stayed Bridge
Effect of Support Conditions on Static Behavior of 1400m main span and 700m side span Cable-stayed Bridge Prof. G. M. Savaliya Department of Civil Engineering Government Engineering College, Surat, Gujarat,
More informationENGR : Roller Coaster Project
ENGR1182.01: Roller Coaster Project P. 1 Roller Coaster Project As part of the project in ENGR1182.01, your team will: Innovate, Design, Build, Document, Test a model roller coaster. To obtain these deliverables,
More informationTechnical Blade Specification for LM 48.8 P rotor blade
Project : LM 48.8 P Document type :Technical Blade Specification Blade item number : 017545-02 Document no. / rev. : BS-00081/A2 Client : Fuhrlander Eng Change ID : 27486/A Number of pages : 10 Date :
More informationMontana Canvas Tent Structure Design
Montana Tech Library Digital Commons @ Montana Tech Proceedings of the Annual Montana Tech Electrical and General Engineering Symposium Student Scholarship 2016 Montana Canvas Tent Structure Design Eric
More informationTechnology that Matters
Angle of Attack (AOA) Indicator Technology that Matters System Description Unique patent-pending technology for Aspen Evolution Calculates AOA from flight envelope data received from AHRS, air data computer
More informationSimulating Airbags for ExoMars Project Using Grids for Competitive Advantage Where Is Your Performance Data?
An Altair Engineering, Inc. Publication W I N T E R 2 0 0 6 2 8 18 Simulating Airbags for ExoMars Project Using Grids for Competitive Advantage Where Is Your Performance Data? Ideas and Strategies in Product
More informationWright Stuff Glider Competition
MESA DAY CONTEST RULES 2018 2019 (Version 9.13.18) Wright Stuff Glider Competition LEVEL: Grades 6 and 7/8 TYPE OF CONTEST: COMPOSITION OF TEAM: NUMBER OF TEAMS: Team 2-3 students per team Preliminary
More informationAIRBUS FlyByWire How it really works
AIRBUS FlyByWire How it really works Comparison between APOLLO s and Phoenix PSS Airbus FlyByWire implementation for FS2002 Copyright by APOLLO Software Publishing The FlyByWire control implemented on
More informationSafety Analysis of the Winch Launch
Safety Analysis of the Winch Launch Trevor Hills British Gliding Association and Lasham Gliding Society ts.hills@talk21.com Presented at the XXVIII OSTIV Congress, Eskilstuna, Sweden, 8-15 June 26 Abstract
More informationPhysics Is Fun. At Waldameer Park! Erie, PA
Physics Is Fun At Waldameer Park! Erie, PA THINGS TO BRING: Amusement Park Physics Bring a pencil Bring a calculator Don t forget to bring this assignment packet Bring a stop watch, a digital watch, or
More informationIntroduction...COMB-2 Design Considerations and Examples...COMB-3
SECTION DIRECTORY General Information Introduction...COMB-2 Design Considerations and Examples...COMB-3 Combination Assembly Recommendations and Limitations Composite Configurations...COMB-4 Typical Sealant
More informationWingsuit Design and Basic Aerodynamics 2
WINGSUIT DESIGN AND BASIC AERODYNAMICS 2 In this article I would like to expand on the basic aerodynamics principles I covered in my first article (Wingsuit Flying Aerodynamics 1) and to explain the challenges
More informationThe Hamburger. by Benjamin Wing Will Bullock Ted Kocak
The Hamburger by Benjamin Wing Will Bullock Ted Kocak December 6, 2008 Abstract The goal is to make a roller coaster that lasts fifteen seconds with a budget of forty dollars. The roller coaster should
More information! "#$ #%& Challenge the future. Delft University of Technology
! "#$ #%& Delft University of Technology One of the biggest challenges for future aviation is represented by the increasing '((. The demand of air transportation is steadlyincreasing, while the constraints
More informationMESA DAY CONTEST RULES (Revised 12/7/17)
LEVEL: Grades 9 12 MESA DAY CONTEST RULES 2017-2018 (Revised 12/7/17) Wright Turn Glider Competition TYPE OF CONTEST COMPOSITION OF TEAM NUMBER OF TEAMS SPONSOR: OVERVIEW: Team 2-3 students per team 9
More informationGain-Scheduled Control of Blade Loads in a Wind Turbine-Generator System by Individual Blade Pitch Manipulation
Proceedings of WindEurope Summit 2016 27 29 SEPTEMBER, 2016, HAMBURG, GERMANY Gain-Scheduled Control of Blade Loads in a Wind Turbine-Generator System by Individual Blade Pitch Manipulation Tetsuya WAKUI,
More informationMotion 2. 1 Purpose. 2 Theory
Motion 2 Equipment Capstone, motion sensor, meter stick, air track+ 2 gliders, 2 blocks, and index cards. Air Tracks In this experiment you will be using an air track. This is a long straight triangular
More information4. Serrated Trailing Edge Blade Designs and Tunnel Configuration
Chapter 4: Serrated Trailing Edge Blade Designs 97 CHAPTER FOUR 4. Serrated Trailing Edge Blade Designs and Tunnel Configuration 4.1 Introduction To evaluate the effectiveness of trailing edge serrations
More informationTHE EFFECT OF LATERAL CONFIGURATION ON STATIC AND DYNAMIC BEHAVIOUR OF LONG SPAN CABLE SUPPORTED BRIDGES
International Journal of Civil Engineering and Technology (IJCIET) Volume 6, Issue 11, Nov 2015, pp. 156-163, Article ID: IJCIET_06_11_016 Available online at http://www.iaeme.com/ijciet/issues.asp?jtype=ijciet&vtype=6&itype=11
More informationPre-lab questions: Physics 1AL CONSERVATION OF MOMENTUM Spring Introduction
Introduction You have a summer job at Amtrak with a group examining the crash between two trains. Your supervisor wants you to calculate the results of two different cases. The first is a perfectly inelastic
More informationTHE INFLUENCE OF CABLE SAG ON THE DYNAMIC BEHAVIOUR OF CABLE-STAYED SUSPENSION BRIDGE WITH VARIABLE SUSPENSION TO MAIN SPAN RATIO
THE INFLUENCE OF CABLE SAG ON THE DYNAMIC BEHAVIOUR OF CABLE-STAYED SUSPENSION BRIDGE WITH VARIABLE SUSPENSION TO MAIN SPAN RATIO G. M. Savaliya 1, A. K. Desai 2, S. A. Vasanwala 3 1 Assistant Professor,
More informationA Study on Berth Maneuvering Using Ship Handling Simulator
Proceedings of the 29 IEEE International Conference on Systems, Man, and Cybernetics San Antonio, TX, USA - October 29 A Study on Berth Maneuvering Using Ship Handling Simulator Tadatsugi OKAZAKI Research
More informationMESA DAY CONTEST RULES
LEVEL: Grades 6-8 Wright Stuff Glider Competition MESA DAY CONTEST RULES 2017-2018 TYPE OF CONTEST COMPOSITION OF TEAM NUMBER OF TEAMS SPONSOR: OVERVIEW: Individual/Team 2-3 students per team 6TH; 2-3
More informationPROGRESS ON THE DESIGN STUDIES OF THE 300AMeV SUPERCONDUCTING CYCLOTRON
PROGRESS ON THE DESIGN STUDIES OF THE 300AMeV SUPERCONDUCTING CYCLOTRON Mario Maggiore on behalf of R&D Accelerator Group Laboratori Nazionali del Sud Catania, Italy CYCLOTRONS 2007, Giardini Naxos, Italy,
More informationMotivations, Opportunities and Challenges of Additive Manufacturing for Space Application
Motivations, Opportunities and Challenges of Additive Manufacturing for Space Application Franck Mouriaux General Manager Structures RUAG Schweiz AG RUAG Space Dearborn, Mai 6 th 2015 Why AM? design complexity
More informationMANUAL REVISION TRANSMITTAL Manual 165A ( ) Illustrated Tool and Equipment Manual. REVISION 21 dated October 2017
HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4215 MANUAL REVISION TRANSMITTAL Manual (61-00-65) Illustrated Tool and Equipment Manual REVISION
More informationNames of Lab Team Members. Scorpion Worksheet
PRE-IB PHYSICS GROUP # Name: DEVIL PHYSICS Period: Date: BADDEST CLASS ON CAMPUS PHYSICS DAY AT BUSCH GARDENS General Guidelines: 1. Data collection is a group effort among your lab team. Completion of
More informationOPTIMUM ANCHORING FOR LONG SPAN CABLE-STAYED BRIDGES
[PROC. OF JSCE Structural Eng./Earthquake Eng. Vol. 1, No. 2 October 1984] OPTIMUM ANCHORING FOR LONG SPAN CABLE-STAYED BRIDGES By Hisanori OHTSUKA*, Toshiaki OHTA** and Fujio IMAI*** This paper presents
More informationAiMT. Flight Trajectory Modelling to Increase General Aviation Safety. Advances in Military Technology Vol. 6, No. 1, June 2011
AiMT Advances in Military Technology Vol. 6, No. 1, June 2011 Flight Trajectory Modelling to Increase General Aviation Safety J. Salga 1* and D. Maturkanič 2 1 Department of Aircraft and Rocket Technology
More informationAdvanced Flight Control System Failure States Airworthiness Requirements and Verification
Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 80 (2014 ) 431 436 3 rd International Symposium on Aircraft Airworthiness, ISAA 2013 Advanced Flight Control System Failure
More informationOverview of Boeing Planning Tools Alex Heiter
Overview of Boeing Planning Tools Alex Heiter Istanbul Technical University Air Transportation Management M.Sc. Program Network, Fleet and Schedule Strategic Planning Module 16: 31 March 2016 Lecture Outline
More informationMechanics of Frisbee Throwing
16-741 Mechanics of Manipulation Project Report Mechanics of Frisbee Throwing Debidatta Dwibedi (debidatd) Senthil Purushwalkam (spurushw) Introduction Frisbee is a popular recreational and professional
More informationTidland Class II Razor Cartridge
TIDLAND SLITTING SOLUTIONS Tidland Class II Razor Cartridge Installation and Operation EN MI 755910 1 This document is for use with Tidland Performance Series Knifeholder Manuals Automatic, Manual or Crush
More informationThe Past, Present, and Future of Nortek and Glider Measurements
The Past, Present, and Future of Nortek and Glider Measurements Peter J. Rusello Scientist Nortek Since 2005, Nortek has collaborated with leading researchers to develop specialized acoustic Doppler current
More informationGlossary. basic empty weight (GAMA). Standard empty weight plus optional equipment.
Glossary General Aviation Manufacturers Association (GAMA) 14 CFR, Part 121. The Federal regulations governing domestic, flag, and supplemental operations. 14 CFR, Part 135. The Federal regulations governing
More informationPropellers. Modeling Conforming Folding. OpenVSP Workshop PM Thursday, August 31, Joseph Derlaga NASA LaRC, CAB
Modeling Conforming Folding Propellers OpenVSP Workshop 2017 1 PM Thursday, August 31, 2017 Brandon Litherland NASA LaRC, ASAB Michael Patterson NASA LaRC, ASAB Joseph Derlaga NASA LaRC, CAB Nicholas Borer
More informationFlying Banners. Shape & Size. Material & Pole Sleeve. Mounting Accessories PROJECTING SIGNS & FLAGS
Flying Banners View our comprehensive range of poles, flags and accessories. Over the next few pages you will find the full range of options - with detailed descriptions on banner shapes and size specifications
More informationHigh School Lesson Glider Design
High School Lesson Glider Design Description Glider Design is the production of gliding products without the use of engines as demonstrated by the NASA space shuttle s return to the Earth s surface after
More informationAn Analysis of Dynamic Actions on the Big Long River
Control # 17126 Page 1 of 19 An Analysis of Dynamic Actions on the Big Long River MCM Team Control # 17126 February 13, 2012 Control # 17126 Page 2 of 19 Contents 1. Introduction... 3 1.1 Problem Background...
More informationAn Analysis of the Restraint Sufficiency of the Happijac Tie-Down System for Truck- Mounted Slide-In Campers
Product Assessment Report October 2002 An Analysis of the Restraint Sufficiency of the Happijac Tie-Down System for Truck- Mounted Slide-In Campers Spencer P. Magleby, PhD Associate Professor of Mechanical
More informationARCTIC/ICE OPERATIONS SESSION. DYPIC A Multinational R&D Project of DP Technology in Ice
Return to Session Menu DYNAMIC POSITIONING CONFERENCE October 9-10, 2012 ARCTIC/ICE OPERATIONS SESSION DYPIC A Multinational R&D Project of DP Technology in Ice Peter Jochmann DYPIC Coordinator Hamburg
More informationAirport Compatibility Brochure 737 MAX
Airport Compatibility Brochure 737 MAX Specific airport compatibility questions concerning Boeing commercial aircraft should be forwarded to: June 2017 BOEING is a trademark of Boeing Management Company.
More informationPRIMARY EDUCATION PACK PROBLEM SOLVING
PRIMARY EDUCATION PACK www.titanclydebank.com Titan Problem Solving 1 The above picture represents a section of the Titan Crane. In constructing this section the materials listed below were used: 2 beams
More informationAlpha Systems AOA Classic & Ultra CALIBRATION PROCEDURES
Alpha Systems AOA Calibration Overview The calibration of the Alpha Systems AOA has 3 simple steps 1.) (On the Ground) Zero calibration 2.) (In-flight) Optimum Alpha Angle (OAA) calibration 3.) (In-flight)
More informationAircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 12 Design of Control Surfaces. Tables
Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 12 Design of Control Surfaces Tables No Term 1 Trim, balance, equilibrium Definition When the summations of all forces exerting
More informationPotential Procedures to Reduce Departure Noise at Madrid Barajas Airport
F063-B-011 Potential Procedures to Reduce Departure Noise at Madrid Barajas Airport William J. Swedish Frank A. Amodeo 7 January 2001 The contents of this material reflect the views of the authors, and
More informationToll Booth. Build a toll booth with an arm that raises and lowers. This does not need to be very large.
Toll Booth Task: You must design, build, and test a toll both that has a gate arm that raises and lowers to let cars through. The toll gate arm will be operated using limit switches to detect whether or
More informationFLIGHT ENDURANCE. Participants analyze flight principles with rubber band powered model aircraft.
Page 1 of 5 OVERVIEW Participants analyze flight principles with rubber band powered model aircraft. PURPOSE The Flight Endurance event requires participants to build, fly, and adjust (trim) a model to
More informationWake Encounter In-Situ Flight Tests in Cruise - Wake Characterization
Wake Encounter In-Situ Flight Tests in Cruise - Wake Characterization Dietrich Fischenberg Carsten Schwarz DLR - Institute of Flight Systems Braunschweig, Germany DLR Weather & Flying Final Colloquium
More informationBoeing Airplane Overview
Boeing Airplane Overview Yonglian Ding, PE Boeing Airport Compatibility Engineering Nov 29, 2016 BOEING is a trademark of Boeing Management Company. Copyright 2016 Boeing. All rights reserved. Agenda Aircraft
More informationTowards Autoomous ISR by a Team of Coopera;ng Gliders
Towards Autoomous ISR by a Team of Coopera;ng Gliders Isaac Kaminer Department of Mechanical and Aerospace Engineering Naval Postgraduate School e-mail: kaminer@nps.edu Joint work with: N. Camacho, B.
More informationBoeing Aircraft and the Impact on Airports
International Civil Aviation Organization on Pavement Management Systems Lima, Peru November 19-22, 2003 Boeing Aircraft and the Impact on Airports Orest Shepson Principal Engineer - Airport Technology
More informationCASM electric cylinders The modular electric cylinder system
CASM electric cylinders The modular electric cylinder system CASM electric cylinders are ideally suited to performing fast and powerful linear movements. Unlike pneumatic or hydraulic cylinders, CASM electric
More informationAirport Compatibility Brochure 737 MAX. March 2014 PRELIMINARY
Airport Compatibility Brochure 737 MAX March 2014 BOEING is a trademark of Boeing Management Company. Copyright 2013 Boeing. All rights reserved. PRELIMINARY Specific airport compatibility questions concerning
More informationENDURANCE GLIDER. Charles R. O Neill School of Mechanical and Aerospace Engineering Oklahoma State University Stillwater, OK 74078
ENDURANCE GLIDER Charles R. O Neill School of Mechanical and Aerospace Engineering Oklahoma State University Stillwater, OK 74078 MAE 4283 Design Project Stability and Control Nov 6, 2000 Endurance Glider
More informationBig SHOT III Hybridization Oven
Big SHOT III Hybridization Oven Models 230402 and 230402-2 Whether you are working with Northern Blots, Southern Blots, Microarrays or another application that requires incubation, you will find the Big
More informationAUTONOMOUS FLIGHT CONTROL AND GUIDANCE SYSTEM OF ACCIDENT AIRCRAFT
24 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AUTONOMOUS FLIGHT CONTROL AND GUIDANCE SYSTEM OF ACCIDENT AIRCRAFT Shinji Suzuki*, Fumihiro Kawamura**, Kazuya Masui** *The University of Tokyo,
More informationo " tar get v moving moving &
Introduction You have a summer job at Amtrak with a group examining the crash between two trains. Your supervisor wants you to calculate the results of two different cases. The first is a perfectly inelastic
More informationIT S NOT ALL BAD NEWS
IT S NOT ALL BAD NEWS 2012 FTSW Seattle, Washington Rodrigo (Rod) Huete President Flight Test & Safety Consultants, LLC Flight Test & Safety Consultants, LLC GOOD SAFETY VS BAD SAFETY Flight Test & Safety
More informationWing Taper Ratio. Wing Incidence. Wing Incidence
Wing Design II Lift surfaces/devices Control surfaces Ailerons Leading-edge slats Vertical Stabilizer Rudder Spoilers Elevators Flaps Horizontal Stabilizer Wing Wing-tip device Basic Configuration Choices
More informationData Sheet for Precision Potentiometer
The ALI(R)17/19 potentiometers in mm housing are suitable for applications where a precise multiturn potentiometer increased radial shaft loads is important. ALI(R)17/19 reinforced bearing ALI(R)17/19
More informationROLLER COASTER POLYNOMIALS Due: Thursday, March 30th
ROLLER COASTER POLYNOMIALS Due: Thursday, March 30th Purpose: In real life, polynomial functions are used to design roller coaster rides. In this project, you will apply skills acquired in Unit 3 to analyze
More informationEvaluating the Robustness and Feasibility of Integer Programming and Dynamic Programming in Aircraft Sequencing Optimization
Evaluating the Robustness and Feasibility of Integer Programming and Dynamic Programming in Aircraft Sequencing Optimization WPI Advisors Jon Abraham George Heineman By Julia Baum & William Hawkins MIT
More informationTechnical Report. Aircraft Overflight and Noise Analysis. Brisbane, California. December Prepared by:
Aircraft Noise Abatement Office Technical Report Aircraft Overflight and Noise Analysis Brisbane, California Prepared by: P.O. Box 8097 San Francisco, California 94128 (650) 821-5100 Introduction In response
More informationPRODUCT PRESENTATION R-BUS. The great traveller
The great traveller APPROACH The R-Bus is Niviuk s first PPG tandem wing suitable for heavy trike use but it can also be used for standard equipment and PPG tandem flights: Robust structure, up to 500
More informationPERFORMANCE MEASURE INFORMATION SHEET #16
PERFORMANCE MEASURE INFORMATION SHEET #16 ARROW LAKES RESERVOIR: RECREATION Objective / Location Recreation/Arrow Lakes Reservoir Performance Measure Access Days Units Description MSIC 1) # Access Days
More informationUC Berkeley Working Papers
UC Berkeley Working Papers Title The Value Of Runway Time Slots For Airlines Permalink https://escholarship.org/uc/item/69t9v6qb Authors Cao, Jia-ming Kanafani, Adib Publication Date 1997-05-01 escholarship.org
More informationAERONAUTICS An Educator s Guide with Activities in Science, Mathematics, and Technology Education National Aeronautics and Space Administration
AERONAUTICS An Educator s Guide with Activities in Science, Mathematics, and Technology Education National Aeronautics and Space Administration Objective The students will: Learn how to change the flight
More informationHelicopter Vector IFR
Helicopter Vector IFR Gerry Wiseman IFR Survey Manager Contents What is IFR? Land IFR Method Dynamic IFR Survey Helicopter IFR Survey Northern Alberta Project MWD Relies on the Earth s Magnetic Field MWD
More informationAustralian Forestry Contractors Association Tasmanian Logging Tilt Test
Australian Forestry Contractors Association Tasmanian Logging Tilt Test Author: Jonathan Vila BEng Reviewed: Sean Carlson BEng CPEng RPEQ Date: 11/12/2018 Issue: Issue 2 File Number: E1073 Executive Summary
More informationNASA S SPACE GRANT MIDWEST HIGH-POWER ROCKET COMPETITION THE ROLL/ORIENTATION CHALLENGE
NASA S SPACE GRANT 2017-2018 MIDWEST HIGH-POWER ROCKET COMPETITION THE ROLL/ORIENTATION CHALLENGE SPRING 2018 COMPETITION LAUNCH HOSTED BY THE MN SPACE GRANT CONSORTIUM AND BY TRIPOLI MN Informational
More informationAeronautics & Air Transport in FP7
Aeronautics & Air Transport in FP7 Liam Breslin DG RTD-H.3 - Aeronautics Brussels, 8 th February 2007 2000 European Aeronautics: A Vision for 2020 2002 Strategic Research Agenda Six Challenges for Aeronautics
More informationAir Traffic Complexity: An Input-Output Approach. Amy R Pritchett, Keumjin Lee and Eric JM Feron School of Aerospace Engineering Georgia Tech
Air Traffic Complexity: An Input-Output Approach Amy R Pritchett, Keumjin Lee and Eric JM Feron School of Aerospace Engineering Georgia Tech Motivation Efforts to balance air traffic demand and airspace
More information2. In terms of forces, explain why Batman The Ride uses a long shallow climb up the first incline instead of a short steep one.
QUALITATIVE QUESTIONS Batman The Ride 1. When you enter Batman The Ride, you walk the first 7.2 meters vertically to get on. What is the advantage to Six Flags St. Louis of having you do this? 2. In terms
More informationTruPunch 1000 and TruMatic 1000 fiber. The first machine concept that grows with you. Machine tools/power tools Laser technology/electronics
TruPunch 1000 and TruMatic 1000 fiber The first machine concept that grows with you Machine tools/power tools Laser technology/electronics 2 Starting out and scaling up TruPunch 1000 and TruMatic 1000
More informationMetal & Teflon Lined Hose
May 2001 Metal & Teflon Lined Hose Components & Controls, Inc. 493 Washington Avenue Carlstadt, NJ 07072 201-438-9190 212-564-5541 Fax: 201-438-3356 www.componentsandcontrols.com Components & Controls,
More informationData Sheet for Precision Potentiometer
AL(R)17/19 soldering lugs The AL(R)17/19 potentiometers in 22 mm housing are suitable for applications where a precise and economical multiturn potentiometer is important. Economical and precise multiturn
More informationn FixtureBuilder is a 3D fixture modeling software that creates R&R setups for documenting and off-line programming. See page 22.
Ability To Inspect Every Detail Many times with traditional fixturing, features can be obstructed from the probe path due to cumbersome and bulky fixturing. With the R&R Fixture, various component and
More informationA A A T E C H N O L O G Y
A A A T E C H N O L O G Y & SPECIALTIES CO., INC. H A R D W A R E C A T A L O G TOTAL SOLUTION SERVICE For the Industrial Piping Marketplace 2011 www.aaatech.com 4 0 Y E A R S S E R V I N G I N D U S T
More informationTakeoff/Climb Analysis to Support AEDT APM Development Project 45
FAA CENTER OF EXCELLENCE FOR ALTERNATIVE JET FUELS & ENVIRONMENT Takeoff/Climb Analysis to Support AEDT APM Development Project 45 Project manager: Bill He, FAA Lead investigator: Michelle Kirby, Georgia
More informationInternational Civil Aviation Organization CHINA RMA REPORT. (Presented by the China RMA) SUMMARY
International Civil Aviation Organization RASMAG/17 WP15 28-31/8/2012 The 17 th Meeting of the Regional Airspace Safety Monitoring Advisory Group (RASMAG/17) Bangkok, Thailand, 28 31 August 2012 Agenda
More informationMANUFACTURING EFFICIENCY
Inch Ball Lock Compatability Chart - Steel Part Part 49605 49606 49607 49608 49601 49602 49611 49612 49621 49622 49631 49632 49633 49634 49641 49642 49643 49644 49705 49706 49707 49708 49701 49702 49711
More information7.1 General Information. 7.2 Landing Gear Footprint. 7.3 Maximum Pavement Loads. 7.4 Landing Gear Loading on Pavement
7.0 PAVEMENT DATA 7.1 General Information 7.2 Landing Gear Footprint 7.3 Maximum Pavement Loads 7.4 Landing Gear Loading on Pavement 7.5 Flexible Pavement Requirements - U.S. Army Corps of Engineers Method
More informationMODELING YOUR FUTURE IN AVIATION Official Air Youth course in elementary aeronautics
MODELING YOUR FUTURE IN AVIATION Official Air Youth course in elementary aeronautics By CHARLES H. GRANT LESSON 9 Planning and building an elementary contest glider THE first model described in this series
More informationJanuary 2018 Air Traffic Activity Summary
January 2018 Air Traffic Activity Summary Jan-2018 Jan-2017 CY-2018 CY-2017 Passengers 528,947 505,421 4.7% 528,947 505,421 4.7% Passengers 537,332 515,787 4.2% 537,332 515,787 4.2% Passengers 1,066,279
More informationKiffin s Crazy Coaster
Kiffin s Crazy Coaster By Orazi s Angels Tyler Kiste, Cory Winters, Michael Dehart Abstract 1 This experiment looked to develop our abilities to work as a team and pushed us to apply the concepts that
More informationSYLLABUS INTRODUCTION TO ROTARY WING FLYING QUALITIES AND PERFORMANCE
22783 Cedar Point Road, Building 2168 Patuxent River, MD 20670 Phone: 301 757 5049 301 757 2731 Fax: 301 342 5003 www.navair.navy.mil/nawcad/usntps SYLLABUS INTRODUCTION TO ROTARY WING FLYING QUALITIES
More informationMath 3 Polynomials Project
Math 3 Polynomials Project ROLLER COASTER POLYNOMIALS Application Problems and Roller Coaster Design due NO LATER THAN FRIDAY, JAN 13. Projects handed in after this date will receive a 0. Purpose: In real
More informationPHY 133 Lab 6 - Conservation of Momentum
Stony Brook Physics Laboratory Manuals PHY 133 Lab 6 - Conservation of Momentum The purpose of this lab is to demonstrate conservation of linear momentum in one-dimensional collisions of objects, and to
More informationMathcad 140 Curriculum Guide
Mathcad 140 Curriculum Guide Live Classroom Curriculum Guide Mathcad 14.0 Essentials Using Advanced Programming Techniques with Mathcad 14.0 Using Advanced Plotting Techniques with Mathcad 14.0 Configuring
More informationThe Development and Analysis of a Wind Turbine Blade
ME 461: Finite Element Analysis Spring 2016 The Development and Analysis of a Wind Turbine Blade Group Members: Joel Crawmer, Edward Miller, and Eros Linarez Department of Mechanical and Nuclear Engineering,
More informationProject 6 Roller Coaster
Project6 RollerCoaster The Folded Paper Ramp/Tube Roller Coaster of Ultimate Domination 6 December 2008 Mohammad Salehi Jay Lockaby Kyle Elich Danny Holbert All members of this group have read and approve
More informationJournal of Aeronautics & Aerospace
Journal of Aeronautics & Aerospace Engineering Journal of Aeronautics & Aerospace Engineering Ahmed Soliman M.Sherif, J Aeronaut Aerospace Eng 217, 6:1 DOI: 1.4172/2168-9792.118 Research Article Open Access
More informationComparison Study between Vault Seismometers and a New Posthole Seismometer
Comparison Study between Vault Seismometers and a New Posthole Seismometer Presented in Salt Lake City, Utah at the Seismological Society of America s Annual Meeting, April 2013 250 Herzberg Road, Kanata,
More information