Questions tagged [aerodynamics]
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184 questions
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Optimizing an airfoil for a range of velocities
This is a bit off the cuff. I was watching a video of a performance analyst for cyclists. I'm not that into cycling, but I've been riding more recently and this piqued my interest. One of the things ...
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Mountain bicycle rubber tires - Will I inhale fumes while riding very slowly in an urban environment? CFD experts based answer required
I recently bought new mountain bicycles. In fear of theft, I stored them a medium sized work room inside the apartment. After ~20 minutes the situation was unbearable. Even after opening all the ...
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Aerodynamic force on two objects being pulled apart
Having searched the web and found nothing, I'm asking y'all: Let's say I have two flat surfaces, and I pull them apart quickly. How do I calculate the aerodynamic drag resisting this motion? I'm sure ...
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32" fan blowing through 24" tube
I currently have a 24" chimney fan rated at about 10000 CFM blowing through a 24" tube. If I were to make a cone so that I could install a 32" fan to blow through the same 24" tube,...
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Crossover distance for ballistic missile vs cruise-missile
For payloads of 100kg and 1000kg, what is the cross-over distance at which the weight of the fuel used to travel a certain distance is equal for a ballistic missile and a cruise-missile/plane? Assume ...
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Can the top speed of a wheel propelled vehcile be limited by traction?
Consider an all-wheel-drive (AWD) car in which the reaction forces on all wheels are equal, and the coefficient of friction is uniform across them. Assuming the vehicle is sufficiently light, the ...
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Unsteady change in angle of attack
I am looking at this paper for unsteady propeller blade loading estimation in non-uniform flow. According to the paper, we can estimate the thrust of a propeller blade section in non-uniform flow by ...
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I want to reduce air speed without backpressure
I am setting up a test-bed for an experiment. Here's what I have. A circular car exhaust The gas comes out of the exhaust at a velocity, x. We need to lower the gas velocity to x/3 Conditions The '...
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Recreating a blade in CAD using a data file from Matlab
I'm running a numerical data model of a wind turbine. I know the blade in question is an S814, as described in the NREL documentation here. I have the necessary blade size data in a MATLAB file shown ...
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Building a Peltier module mini-cooler
I am just a noobie in engineering stuff. Should the DC Fan 1 suck the air out of the Al heat sink OR push air into it for more efficient heat dissipation? For the small heat sink placed on the colder ...
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How to determine wedge angles, stagger angles, pitch, and chord for axial turbine mean-line modelling?
I would like to measure the performance and optimize the design of an axial turbine using mean-line modelling. However, most of the optimization codes I found on GitHub require wedge angles, stagger ...
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How should a stationary suspended spherical tube be modified to incorporate aerodynamic downforce mitigating both fore and aft 45 mph - 120 mph winds?
The question involves this topic; High-wind rollover damage in center-pivot irrigation systems. This study involves the additive engineering possibilities to achieving an aerodynamic remedy ...
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How does one calculate the aerodynamic pressure on a spacecraft during Max Q?
Just as lift - off of a spacecraft commences, that spacecraft undergoes aerodynamic pressure. After a certain point, the spacecraft reaches Max Q or maximum aerodynamic pressure. I do know that Max Q ...
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Characteristic scales in Thin Shear Layers Equations (Aerodynamics)
I am struggling to understand what characteristic scales mean in the context of thin shear layer equations. I am referring mostly to the following paragraph from the book "Turbulent Shear Layers ...
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How could I calculate the torque due to lift and drag in the body frame?
I'm trying to figure out the torque due to aerodynamic forces on an aircraft confined to two dimensions (so no sideslip). Defining the windframe with basis vectors $\hat{w_1}, \hat{w_2}$ obtained by ...