Structures and Weights Preliminary Design Review

Slides:

Advertisements

Similar presentations

Aircraft Motion and Control

Advertisements

6th grade Springton Lake

AAE 451 Aircraft Design Aerodynamic Preliminary Design Review #2 Team Members Oneeb Bhutta, Matthew Basiletti, Ryan Beech, Mike Van Meter.

Lesson 13: Aircraft Structures And Flight Controls

Boy Scouts Aviation Merit Badge Control Surfaces.

Airplane Flight: X-Plane in the Classroom Control Pitch - nose moves up and down.

D & C PDR #1 AAE451 – Team 3 November 4, 2003

Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Critical Design Review Team 1.

March 3, Structures and Weights 2 PDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason.

CM 197 Mechanics of Materials Chap 14: Stresses in Beams

November 12, 2003QDR1 Team 5 Structures and Weights QDR #2 Scott Bird Mike Downes Kelby Haase Grant Hile Cyrus Sigari Sarah Umberger Jen Watson.

Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Team 1: Structures 1 PDR Team “Canard” October 12th,

Rear spar for control surface hinges Styrene foam wing core Balsa spars carry bending load 0.25 in x 0.25 in T.E. Reinforcement Materials Employed: Balsa:

March 1, Aerodynamics 3 QDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason Tang Joe.

Over view Landing Gear Landing Gear Weight Determination Weight Determination Geometric Layout of Wing Structure Geometric Layout of Wing Structure Analysis.

Team 5 Aerodynamics PDR Presented By: Christian Naylor Eamonn Needler Charles Reyzer.

DR2 Structures PDR Structures and Weight Preliminary Design Review October 5, 2000 Presented By: Jeff Rodrian & Chris Curtis Team DR2 Loren Garrison Chris.

Team 5 Structures PDR Presented By: Ross May James Roesch Charles Stangle.

CLARKSON UNIVERSITY Department of Mechanical and Aeronautical Engineering Introduction to AIRCRAFT STRUCTURES Ratan Jha (CAMP 364, ,

Minimum Weight Wing Design for a Utility Type Aircraft MIDDLE EAST TECHNICAL UNIVERSITY AE 462 – Aerospace Structures Design DESIGN TEAM : Osman Erdem.

1 AE 440 Structures Discipline Lecture 6 Eric Loth For AE 440 A/C Lecture.

Utilizing your notes and past knowledge answer the following questions: 1) What part of the aircraft is located on the outer portion of the trailing edge.

Leading Cadet Training

Lesson 2-2a Principles of Flight

SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 Design.

Warm-Up – 8/25 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the four forces of flight? Describes what.

The Lumberjacks Team /16/12 Brian Martinez.

Group 10 Dimitrios Arnaoutis Alessandro Cuomo Gustavo Krupa Jordan Taligoski David Williams 1.

ITA – Instituto Tecnológico de Aeronáutica

Ashley Brawner Neelam Datta Xing Huang Jesse Jones

AAE 451 Aircraft Design First Flight Boiler Xpress November 21, 2000

December 1, 2003PDR1 Team 5 Structures and Weights PDR #2 Scott Bird Mike Downes Kelby Haase Grant Hile Cyrus Sigari Sarah Umberger Jen Watson.

February 24, Dynamics & Controls 1 PDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason.

Structures PDR 1 Team Boiler Xpress Oneeb Bhutta Matthew Basiletti Ryan Beech Micheal VanMeter October 12, 2000.

Aircraft Motion and Control

Patrick Dempsey Bridget Fitzpatrick Heather Garber Keith Hout Jong Soo Mok Structures Preliminary Design Review #1 October 12, 2000.

Dynamics & Controls PDR 2

6.01 Aircraft Design and Construction References: FTGU pages 9-14, 27

Vehicle Sizing AAE 451: Team 2 Michael Caldwell Jeff Haddin

STRUCTURES & WEIGHTS PDR 1

Team 3 Structures and Weights PDR 2

Basic Aircraft Structure

Team “Canard” September 28th, 2006

CGS Ground School Principles Of Flight Controls © Crown Copyright 2012

Aerospace System Prototyping and Validation- Lecture 2

Aerodynamics PDR AAE451 – Team 3 October 21, 2003

Structures and Weights

Dynamics & Controls PDR 1

SAE AERO 2017 Joseph Zongolowicz, Kathy Hansen, Nick Montana, Marquis Ward, Frank Dixon, Thomas Houck, Gerald Short, Zhangsiwen Xiao, Kevin Schesventer,

Team One Dynamics and Control PDR 2 10 March, 2005

Structures and Weights 1 QDR

4 2 . Parts of the Airplane.

Warm-Up – 9/5 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the four forces of flight? Describes what.

Aircraft Stability and Control

STRUCTURES & WEIGHTS PDR 2

c/Maj Christopher Greves

Balsa Glider Construction

Dynamics and Control PDR 2

Structures Overview Material Properties Structures Construction

Aether Aerospace AAE 451 September 27, 2006

Structures QDR #2 AAE451 – Team 3 November 13, 2003

Team 5 Structures and Weights QDR #1

Structures and Weights 1 QDR

CAD Design Part 2 AE460 Greg Marien Lecturer.

Structures PDR #1 AAE451 – Team 3 October 28, 2003

Balsa Glider Construction

Aether Aerospace AAE 451 September 19, 2006

Dynamics N Controls 1 PDR

Dynamics & Controls PDR 2

STRUCTURES & WEIGHTS QDR 1

Presentation transcript:

Structures and Weights Preliminary Design Review Phoenix Aerospace – Structures Team Jamie Allen Andy Wiratama 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Objectives Material Properties V-n Diagram Wing Loading Analysis Weight Breakdown CG Locations Wing Layout Analysis and Testing Landing Gear 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Material Properties *note properties are approximate values for average materials, and most are not true constants 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

V-n Diagram 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Wing Loading Analysis MATLAB Code is used to determine: Wing loading using Schrenk’s approximation (Raymer) Trapezoidal Approximation Elliptical Approximation Shear force Moment Centroids 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Wing Loading Analysis Front Wing Loading Rear Wing Loading 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Wing Loading Analysis Front Wing Shear Force Rear Wing Shear Force Shear Force decreases as it moves away from the root to the tip 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Wing Loading Analysis Front Wing Moment Rear Wing Moment Moment about the longitudinal direction Small wing load distribution at tip leads to small moment at the tip 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Weight Breakdown 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

CG Locations X measured from nose to tail (roll axis) CG x=31.37 in. y=0 z=3.32 in. X measured from nose to tail (roll axis) Y measured spanwise from center of fuselage (pitch axis) Z measured vertically from bottom of fuselage (yaw axis) Simplifying Assumptions: Symmetric Rectangular sections using root chord Wings as flat plates 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Wing Layout Shaped using foam Rectangular spars (caps) located around quarter-chord Spar towards trailing edge to support control surfaces Monokote used to strengthen and smooth surface Depending on testing, may add stringers or other strengtheners 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Analysis and Testing Fuselage design Wing layout (program for spar sizing) Wing deflection calculations ViSTA analysis Construct scaled-down wing Sandbag loading test 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001

Landing Gear Taildragger configuration Buy pre-designed gear Tip-over analysis Sizing for gear (trade study) *diagram from Raymer 11/18/2018 Phoenix Aerospace AAE 451 – Fall 2001