Conceptual Design Review

Conceptual Design Review

Supersonix Inc. Conceptual Design Review Of a high speed commercial air transport Akshay Ashok, Nithin Kolencherry, Steve Skare, Michael McPeake, Muhammad Azmi, Richard Wang, Mintae Kim, Dodiet Wiraatmaja, Nixon Lange 4/30/2009 Supersonix Inc. 30 April 2009 Team 2 Conceptual Design Review Table of Contents TABLE OF CONTENTS ........................................................................................................................... 2 TABLE OF FIGURES ............................................................................................................................... 4 LIST OF TABLES ...................................................................................................................................... 6 EXECUTIVE SUMMARY ......................................................................................................................... 7 INTRODUCTION...................................................................................................................................... 8 Opportunity Description ........................................................................................................................................ 8 Mission Statement ................................................................................................................................................. 9 Market Analysis and Concept of Operations .......................................................................................................... 9 SELECTED AIRCRAFT CONCEPT ....................................................................................................... 9 AIRCRAFT DESIGN MISSION ............................................................................................................. 13 AIRCRAFT DETAILED SIZING ........................................................................................................... 14 Primary Functions ................................................................................................................................................ 15 A/C Geometry ......................................................................................................................................................... 15 Mission Segments ................................................................................................................................................... 15 Component Weights ............................................................................................................................................... 16 Overpressure .......................................................................................................................................................... 17 Airfoil and Lift Coefficients ..................................................................................................................................... 17 Constraints .............................................................................................................................................................. 17 Stability ................................................................................................................................................................... 18 Wing Loading .......................................................................................................................................................... 18 Auxiliary Functions .............................................................................................................................................. 18 Engine Modeling ..................................................................................................................................................... 18 Drag Modeling ........................................................................................................................................................ 20 Transonic Drag ..................................................................................................................................................... 24 CARPET PLOT ....................................................................................................................................... 25 AIRCRAFT CONCEPT/DESCRIPTION ............................................................................................. 29 AERODYNAMICS ................................................................................................................................... 32 Airfoil Selection ................................................................................................................................................... 32 Drag Buildup ........................................................................................................................................................ 38 SONIC BOOM .......................................................................................................................................... 40 PERFORMANCE ..................................................................................................................................... 47 V-N Diagram ........................................................................................................................................................ 47 Range Diagram .................................................................................................................................................... 48 PROPULSION ......................................................................................................................................... 48 Inlet ..................................................................................................................................................................... 48 Engine Description ............................................................................................................................................... 50 Page 2 of 72 Supersonix Inc. 30 April 2009 Team 2 Conceptual Design Review Nozzle Design ...................................................................................................................................................... 51 STRUCTURES ......................................................................................................................................... 53 Engine mounting .................................................................................................................................................. 56 Landing gear ........................................................................................................................................................ 56 Material selection ................................................................................................................................................ 57 WEIGHTS AND BALANCE ................................................................................................................... 58 Aircraft Component Weight ................................................................................................................................. 58 STABILITY AND CONTROL ................................................................................................................ 61 Static Longitudinal Stability ................................................................................................................................. 61 Control Surface Sizing .......................................................................................................................................... 62 COST ANALYSIS .................................................................................................................................... 63 RDT&E Cost .......................................................................................................................................................... 63 Direct Operating Costs (DOC) ............................................................................................................................... 64 Indirect Operating Costs (IOC) ............................................................................................................................. 65 Cost Summary...................................................................................................................................................... 66 SUMMARY ............................................................................................................................................... 66 Additional work ................................................................................................................................................... 68 REFERENCES .......................................................................................................................................... 69 APPENDIX............................................................................................................................................... 71 Engine Performance Curves (from Raymer App.E) ............................................................................................... 71 Composite carpet plot ......................................................................................................................................... 72 Page 3 of 72 Supersonix Inc. 30 April 2009 Team 2 Conceptual Design Review Table of Figures Figure 1: Lower Walk-Around (Takeoff Climb Phase) ..................................................................

View Full Text

Details

  • File Type
    pdf
  • Upload Time
    -
  • Content Languages
    English
  • Upload User
    Anonymous/Not logged-in
  • File Pages
    72 Page
  • File Size
    -

Download

Channel Download Status
Express Download Enable

Copyright

We respect the copyrights and intellectual property rights of all users. All uploaded documents are either original works of the uploader or authorized works of the rightful owners.

  • Not to be reproduced or distributed without explicit permission.
  • Not used for commercial purposes outside of approved use cases.
  • Not used to infringe on the rights of the original creators.
  • If you believe any content infringes your copyright, please contact us immediately.

Support

For help with questions, suggestions, or problems, please contact us