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Texas A&M AeroDesign Team 2010!!
October 28 2009
Texas A&M AeroDesign Team 2010!!
What a fantastic year we had last year! Thanks to the support of Model Airplane News and the tireless dedication of the 2009 design team, we were able to accomplish big things with our design project! Our story brought a lot of attention and I am proud to say that this year we are an official University-recognized design group! We recruited members of the sophomore and junior class at Texas A&M for 2010 Aerodesign competition team and were stunned by the shear number of applicants this year! The aerospace department is buzzing with excitement for this year's competition - we couldn't have done it without you and we offer all of our followers our deepest gratitude.This year, our team has grown from 7 members to 14 - every member was competitively selected from a pool of over 50 applicants and I am confident that we will make strides over last year's entry. To date, the team has been busy with conceptual design and initial modeling and simulation on this year's AeroDesign competition entry. Certain aspects of the competition have changed for 2010 including an increased overall aircraft size allowance and the prohibition of certain composite materials such as FRP, etc. Size limitations have increased from a length-width-height measure of 175 inches to 200 inches - we plan on fully taking advantage of this size increase by implementing a longer, higher-lift and higher-aspect-ratio wing, a minimal fuselage, and increased control authority via larger control surfaces and increased aircraft stability. More details to come! Structures Team - November 6, 2009 The structures team has been analyzing ribs and wing structures already decided on the rib spacing and the overall spar design. The original back spar design has just been modified to be able to support the flaps and aileron. We are currently working on the SolidWorks model of the aircraft. We have experienced som issues with the solid modeling program, but we continue to soldier on. We have ben doing FEM structural analysis using ABAQUS and looking for ways to make our structure as light-weight and structurally sound as possible. The plan is to stick to the "laminated" spar we analyzed earlier. More updates to come! Aerodynamics Team Our team has been working hard the past few weeks. Using the program XFLR5, we analyzed a variety of low-Reynolds Number airfoils, comparing values of lift, drag, and wing tip vorticies. After deciding as a group to go forward using the Eppler 216 airfoil, we continued to use XFLR5 to model different wing shapes and planforms, ultimately deciding to use a tappered wing with root chord 18 in and a tip of 14 in. Right now, we are focusing on getting lift and drag numbers to the Structures and Control groups, while also beginnig work on our wind tunnel model, which we plan on running in the next few weeks. Some of the issues we are running into concern programming limitations using XFLR5 to analyze the flow quality around our fuselage, especially when trying to see how much drag our fuselage will create and how much this will affect the lift of our wing simulations. Bottom line, we are trying to gauge how realistic our values are and to determine what to expect once we get to flight testing. Stability and Control: The stability and control team has been focusing on taking the values for CG, AC, moments, etc provided by the propulsion and aerodynamics teams and implementing them into a design for the flaps, ailerons, elevator, and rudders. As of right now, the team has decided on building a "flying wing with a tail" - the tail section would provide a good measure of stability and controlability to an otherwise unstable flying wing platform. We have finished sizing the elevators and rudders - our next task is to size the flaps and ailerons. We are also studying the effects of adding spoilers and speed breaks to our model. SInce the wing will be very large with a very high lift, we think the spoilers and airbreaks would help the plane when it comes in for landing with relatively low weight. Propulsion and Avionics: The propulsion and avionics team's responsibilities include testing and optimizing the engine and prop, as well as the overall design of the aircraft control system and radio system. We have designed and built a thrust measuring test stand for thhe engine. Using this stand we have been testing a wide variety of propellers, carb settings, mixture settings, etc to find the combination that provides us with the biggest possible thrust. Since the competition doesn't require long endurance, we can fly the entire circuit at full throttle without a problem. Our top props have been APC and Master Airscrew 13x6's and 14x4's. Hitec RCD has generously donated a radio system - once we receive it we will start servo testing and control system design ***************************************************************************************************************** November 20,2009 Propulsion and Avionics: Prop testing was successful with some minor issues. We had some scares early on with getting our engine to start for every run, but we have effectively overcome that task. The APC props have been the strongest ones we have tested, providing the max allowable thrust, when compared to the Master Airscrew props. Our radio system just came in this week and our team is excited to begin servo testing! With these tests, we will be able to provide data for the stability and control team concerning elevator and rudder positioning for the overall control system design. ***************************************************************************************************************** November 22, 2009 Structures:
We are finally getting detail oriented! The spar is shaping up—we have calculations for its dimensions, and are figuring out the most effective way to build it with the resources we have available. As for the ribs, we have been working with programs such as Abaqus and Maple to aide in their design. These programs have provided for the spacing of the ribs, as well as, a preliminary analysis of the ribs with their predicted loads. ***************************************************************************************************************** November 24, 2009 Structures: The ribs are still being examined to determine where the lightening holes can be made. The support for the engine and fuel tank has now been added to our base plate. We still need to determine where we can make lightening holes on it as well. The goal here is to save as much weight as possible while making our aircraft tough enough to survive flight with a good deal of payload. It has also been decided to have a different spar towards the wing root (wider at the root than the tip) to increase our factor of safety there. The spar layering design is complete and is in the process of being added to our working wing assembly. We have also decided what type of hinge we will use and how it will be attached to our back spar. January 18. 2009 |


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