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Top 10 of the best aircraft design software
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The same applies to things like propellers. It won't give you accurate results. With that said, if you design an aircraft and set the flight conditions within reasonable operating limits, MachUp will give very accurate results. We've compared the results produced by MachUp to both CFD and wind-tunnel tests and MachUp provides very accurate results in a fraction of the time that either CFD or wind tunnel testing would require. It has been used in a multitude of projects, including designing several advanced UAS systems employed by AggieAir for long-range, remote sensing missions.
So, there you have it. Thats your introduction to MachUp.
I hope you enjoyed it and that you will stay tuned for more articles about how to use MachUp. Throughout the whole process of creating MachUp, our goal here at the USU Aerolab has been to put aircraft design into your hands. Now you don't need a PhD to get your hands dirty designing an aircraft. So get out there and make something awesome! You need to log-in to rate articles. Looking for your store account?
So lets get started! Once you get into MachUp, you'll see a window that looks like this: To give you a brief overview, there are basically three steps to using MachUp: Build the airplane Set the flight conditions Run an analysis Now lets dive a bit into each of those steps.
So, first step: Build the airplane. Forces and Moments: Analyzes the forces and moments on the aircraft for the given flight condition. The results are first split into the forces created by the lifting surfaces wings and the props and then they are combined to give the total forces at the bottom. FL is the lift force. FD is the drag force. FS is the side force.
Performance Derivatives: Analyzes how the aerodynamics of the aircraft change with small changes in the flight condition, specifically the angle of attack and sideslip angle. I'll write another article explaining more about this later, but the important bit is this: If your analysis shows these results, small disturbances to the flight condition will not cause your aircraft to flip over.
Also, you want to get the Static Margin as close to 0. This is a measure of the stability and maneuverability of the aircraft and should be used to find the correct placement for the center of gravity CG. Aerodynamic Center: Calculates the aerodynamic center of the aircraft. The aerodynamic center is the point about which changes in the angle of attack do not affect the pitching moment. It is pretty important and used in more advanced aerodynamic calculations, but may not be necessary for what you want to do. Stall Onset: This analysis takes airspeed that you specified in the flight condition and then increases the angle of attack until any part of the aircraft stalls.
It then tells you the stall angle of attack, the amount of lift you can produce at that angle of attack and the specified airspeed right before stalling and the location of the stall. Arguably, the next analysis is probably more useful to you if this sounds interesting.
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Stall Airspeed: Calculates the minimum airspeed that you need to fly based on a specified aircraft weight. This is one of the slowest analyses to run, but also one of the most useful. Essentially, once you have designed your aircraft, you set anticipated weight of your aircraft, and this analysis will tell you how fast you need to be going before you can get off the ground. Also gives the same information as the Stall Onset analysis. Target Lift: Calculates the angle of attack necessary to produce a specified amount of lift at the given airspeed.
Pitch Trim: Calculates the angle of attack and elevator deflection necessary to trim the aircraft for a target lift and moment at the given airspeed. To run this analysis, your aircraft must have an elevator and you must have designed it well enough that it is possible to trim it in pitch. Saves a text file describing the distribution of the forces and moments on the wings and propellers.
Recommend This Article You need to log-in to rate articles. Looks like a nice resource, but for me its not really useful as you only allow Naca airfoils. Most of the airfoils i am using are not naca. It needs to allow you to use any airfoil dat file. Secondly when you are in mach and go to the top menu, all the links to "tutorials" take you to a totally different program tutorial. Log In to reply. Thanks for your feedback! In response to your comments, MachUp has an interesting way of handling airfoils. When you put an airfoil into the 'Airfoil graphics only ' slot, it takes that airfoil name currently only supports NACA 4 digit airfoils and uses it to update the graphics what you are seeing but it doesn't affect the aerodynamics the calculations.
The aerodynamic calculations are only affected by changing the other variables in the 'Airfoil' drop down menu. This video https: Its a bit more advanced, but it sounds like you're looking for something more advanced. So, while the graphics currently can only model NACA airfoils although I do like the idea of using a dat file to make the graphics model other airfoils , in order to actually change the aerodynamics you have to mess with the other variables. Also, I'll look into getting the tutorials link updated.
For now you can find a few tutorials for older versions of MachUp on our YouTube page: Jackson T on June 20, That is one awesome program! Do you think you could do an overview of MachUp4 later on maybe?
I really like aerodynamics and I think this will be a great way to learn more with. Thanks for sharing it with everyone!
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