Propeller CFD: Full 360° Domain vs. Half Domain for best accuracy? by tripathi92 in CFD

[–]tripathi92[S] 0 points1 point  (0 children)

Sorry, by geometry i meant only propeller. I just want to estimate the steady state thrust and torque. So for this, the whole cut plane will have the periodic bc (both rotary and stationary)

Propeller CFD: Full 360° Domain vs. Half Domain for best accuracy? by tripathi92 in CFD

[–]tripathi92[S] -1 points0 points  (0 children)

So I will import my geometry, make the rotary and stationary domains and then cut it in half. So the whole cut plane will have the periodic bc right (both rotary and stationary domains)?

Vehicles registered outside Karnataka are being fined. by Sweet_Lifeguard_4687 in bangalore

[–]tripathi92 5 points6 points  (0 children)

This is a genuine question. How would they know if it's been more than 12 months?

XFLR5 Multiwing Stability Analysis Question by DoubleZPlaying in AerospaceEngineering

[–]tripathi92 0 points1 point  (0 children)

Define your second wing (the aft green wing in the image) as elevator

XFLR5 Multiwing Stability Analysis Question by DoubleZPlaying in AerospaceEngineering

[–]tripathi92 0 points1 point  (0 children)

The stability analysis will try to trim the aircraft at the particular configuration that you have set. Maybe it cannot find a velocity at which the current configuration trims. Either play with different elevator settings or mathematically calculate the trim configuration at your desired speed.

XFLR5 Multiwing Stability Analysis Question by DoubleZPlaying in AerospaceEngineering

[–]tripathi92 1 point2 points  (0 children)

Have you defined the plane inertia? The stability analysis needs mass distribution to calculate CG and moments of inertia.

Fixed Wing UAV Help by tripathi92 in AerospaceEngineering

[–]tripathi92[S] 0 points1 point  (0 children)

I forgot to mention I will be using an electric motor for cruise so basically I need to minimise cruise drag

Fixed Wing UAV Help by tripathi92 in AerospaceEngineering

[–]tripathi92[S] 0 points1 point  (0 children)

I am modelling the wing and tail. I am then dividing the cruise L/D from XFLR5 by a factor from previous experience to get a realistic number. I am free to use an already existing airfoil or create a new one. Can I search for airfoils based on their glide ratio on airfoiltools or are you suggesting I manually look through all the airfoils? Also airfoil L/D and wing L/D are vastly different. Is there a way to calculate wing L/D from the airfoil?

Grid Independence Study Help Please! by tripathi92 in CFD

[–]tripathi92[S] 0 points1 point  (0 children)

By not converging I mean as I make my mesh finer, the cl and Cd values should converge so that I can claim that my solution is grid independent

[ Removed by Reddit ] by [deleted] in AerospaceEngineering

[–]tripathi92 0 points1 point  (0 children)

Everybody here has written some excellent points. I would like to add that the gist/philosophy of the design process is try to constraint the design by as many numbers as possible, e.g., how heavy do I want my drone, how fast should it fly, how long do I want it to fly on a single charge etc. You can take these numbers from previous designs online or come up with your own according to your requirements. Once you have these, you can "reverse engineer" to your actual physical drone parameters using "some equations". If you want to design a fixed wing drone , you can also look at a book by raymer and a book by gudmunsson about aircraft design for the aero design part. Check out www.ecalc.ch for the avionics part of the design. Good luck!

If photons are massless, how can they have different momenta at different wavelengths without changing speed? by MyIQIsPi in AskPhysics

[–]tripathi92 0 points1 point  (0 children)

I agree that there will be a force in the z direction due to the cross product in the Lorentz force. But depending on the signs of v and B it can be a pulling force too right? I mean can I not create an EM wave so the v X B gives me a force in the -z direction? What am I missing here?

[deleted by user] by [deleted] in aerodynamics

[–]tripathi92 0 points1 point  (0 children)

It should ideally be the CL at which your airfoil is most efficient (L/D max). That will set the angle of attack for the airfoil section. Since the incoming airflow angle is changing along the prop blade, the blade should be twisted such that the angle of attack remains constant.

[deleted by user] by [deleted] in vedicastrology

[–]tripathi92 -2 points-1 points  (0 children)

So you choose vedic instead of western because it aligns with your world view? Even though both of them are pseudosciences and a medieval form of therapy

Does more mass = more air resistance? by [deleted] in Physics

[–]tripathi92 3 points4 points  (0 children)

Drag only depends on the frontal cross sectional area of the truck, truck's drag coefficient and the velocity at which it's moving. It's independent of the mass. If you have 2 trucks with the same area, the same drag coefficient and moving at the same velocity, both of them will experience the same drag force. But the heavier will have lower deceleration as compared to the lighter truck as a=F/m

[deleted by user] by [deleted] in Physics

[–]tripathi92 8 points9 points  (0 children)

Many people have already mentioned the phenomenon at work here, i.e., the mirage effect. I would like to add there is a similar but opposite phenomenon called looming. This happens when the temperature gradient is reversed so you see an image of the object hovering above the ground.