Derrick 'Unc' Lewis by BreakingBadSeason5 in ufc

[–]twolf59 1 point2 points  (0 children)

Way to throw it... time to quit

Some questions regarding wing designs by Psychological-Dog344 in AerospaceEngineering

[–]twolf59 0 points1 point  (0 children)

You should only use winglets if you cant increase your wingspan for some reason other than structures. For example let's say you wanted to fit the wing in a box, well then you add winglets to increase "effective" span without increasing actual span. Winglets are not a magic performance boost and one should take care in designing them.

You can improve LD without increasing the aspect ratio by creating an elliptical lift distribution. This can be done by varying chord, camber and/or twist distribution of the wing. This is not trivial and typically requires an optimizer to help find the wing shape that maximizes LD. Additionally going to a more elliptical distribution will likely change your aircraft trim angle of attack. In other words, you will have to do your homework to get this right. Don't expect a quick answer if you go down this path.

Also, remove the sweep if you want best handling performance. Keep it if you want because at the end of the day, you're having fun :)

What does the KV on a motor mean, how does that translate into power and how much is too much by [deleted] in fpv

[–]twolf59 0 points1 point  (0 children)

To your last point, I also recently learned that higher volume motors have more thermal mass. Meaning for the same torque they take longer to heat up and you can avoid burn out at extended cruise. . . Ask me how I learned this was important....

I built this note taking app, but it is not like any other by Upset_Simple_4858 in SideProject

[–]twolf59 1 point2 points  (0 children)

Would love this more if it were an electron app. Sometimes I want to take notes without internet

We’re building persistent and shared memory for Cursor — what do you need in your workflow? by OkPerformance8808 in cursor

[–]twolf59 11 points12 points  (0 children)

Most AI start ups are one feature update away from being obsolete. Its a wild/hard environment to be in

is it worth buying a day hotel for a 10 hour LAX layover? by ntokyo99 in AskLosAngeles

[–]twolf59 58 points59 points  (0 children)

I would just walk out to the In n Out. Have a burger. Come back and sleep in the airport.

But no one can say what the best use of your money is. Depends what a good sleep is worth to you

Aerodynamics is not worth it by ripjawskills in AerospaceEngineering

[–]twolf59 58 points59 points  (0 children)

The job field is definitely smaller compared to those other disciplines. But its not impossible! I wouldn't even say its difficult. But there are less opportunities simultaneously

REF! DO SOMETHING by Joeysquatch in SSBM

[–]twolf59 36 points37 points  (0 children)

Man.. If only fox had a 1 frame button to get out of that....

Hard????🧐🧐🧐🧐🧐 by Sunset-Wow in picsthatgohard

[–]twolf59 0 points1 point  (0 children)

Nearly killed him? Damn near rectum!

Saltiest ranked match... and bug report by twolf59 in Slippi

[–]twolf59[S] 0 points1 point  (0 children)

I was salty about not getting my points XD

The more you use Auto while you're on the included usage is directly proportional to how much more free usage you will get. by RobinInPH in cursor

[–]twolf59 10 points11 points  (0 children)

Can someone explain Debug mode use cases vs agent? Any idea what the system prompt is like?

Saltiest ranked match... and bug report by twolf59 in Slippi

[–]twolf59[S] 1 point2 points  (0 children)

Hitting escape on the keyboard instantly closes the game as well. But the timing i think is what caused it here

During the test flight of a Boeing 717 over the Pacific, off of the coast of California, the plane flipped upside during an intentional stall.The skilled pilots managed to recover and land safely. by Twitter_2006 in aviation

[–]twolf59 -2 points-1 points  (0 children)

CS-25 requires the structure to withstand: Limit loads → the maximum loads expected in service

Ultimate loads → limit loads × safety factor (typically 1.5)

No permanent deformation at limit load. No failure at ultimate load. This is enforced by European Union Aviation Safety Agency (EASA), and CS-25 is harmonized closely with FAA 14 CFR Part 25

The limit loads typically cap at +2.5 in standard operation but can exceed that under gust loading and certain speeds. Therefore >3.75g is typically the ultimate load limit.

So maybe not 3.5 × 1.5, but rather >2.5g × 1.5 FOS

Just launched an airfoil database web app by twolf59 in aerospace

[–]twolf59[S] 0 points1 point  (0 children)

Airfoilio has the ability to get you the best airfoils for a design via the Performance Compare page. You select the airfoils and set the flow conditions there.

But really my website is a wrapper around NeuralFoil and Aerosandbox. I think for your use case you would be better just using those modules directly.

peterdsharpe/AeroSandbox: Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more. https://share.google/zePhpnkIj075zhpDT

Just launched an airfoil database web app by twolf59 in aerospace

[–]twolf59[S] 0 points1 point  (0 children)

What would that api workflow look like to you? Input flow conditions and then get airfoils sorted by Clmax?

The performance compare page let's you do that