r/AerospaceEngineering • • 22d ago

Uni / College Monthly Megathread: Career & Education: Post your questions here

0 Upvotes

Career and Education questions should go here.


r/AerospaceEngineering • • 4h ago

Personal Projects Made an open-source GUI based on openfoam

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58 Upvotes

I thought this was cool and wanted to share it here, This here is a NACA 0012 wing at 8° run in it The mesh is about 149k cells with a wake refinement box and 3 prism layers. The particles are coloured by pressure, and you can see the suction peak and the tip flow.

Anyway I wanted to show it because I finally believe it is a bit presentable now, it is basically a gui with openFOAM, and additionally I added TENO schemes from Fu et al, I thought of adding higher order schemes for more accuracy.

Most of the code is human slop, otherwise known as "spaghetti code" I have yet to clean it up so apologies for any bugs that may arise.

Source code: https://github.com/CakeCFD/cake-studio

Website: https://cakecfd.org/

note that a variant of this post was also posted in r/CFD

I would like opinions from fellow engineers on how to improve this further and make this better, or more specifically what validation case would you trust before using the TENO schemes?


r/AerospaceEngineering • • 2h ago

Discussion Question about take-off weight calculation for Aircraft Design based on M. Sadraey book

3 Upvotes

So I'm currently helping my friend designing some UAV cargo aircraft like the HH-200 from China and I found some difficulties regarding take-off weight calculation for this aircraft.
For the context, the UAV is not small like a typical UAV but rather large in size.

Fig 1. HH-200

And so for these UAV, my friend decided to make an UAV cargo similar to these. The UAV will only use single engine (turboprop engine) and this where it start to make a problem.

So in these section, Sadraey explain that the equation used is the equation on 4.26. He explain that the a and b value is obtained from the table 4.8 that based on data he obtained.

Fig 2. The equation used to find the We/Wto
Fig 3. Formula used to calculate the takeoff weight
Fig 4. Table 4.8 which show the a and b value

Because there are no UAV classification yet in the table 4.8, he use the a and b value for General Aviation with single engine. I also think that the GA-single engine classification is the closest one we know for his UAV design. The a and b value is presented on table 4.8

When he calculate the take-off weight for the aircraft, the output from the formula does not generate a convergent value at all presented by the image below.

Fig 5. The output from the formula

I also have tried to check the formula using quadratic formula from the his 2nd edition book about Aircraft Design and only getting this.

Fig 6. Checking with quadratic formula

The take-off weight showing error because the value inside the square root is negative thus the quadratic formula can't be solved.

But when we change the a value from positive to negative, all of the equation resulting in normal result like these one.

Fig 7. Change the value a from positive to negative

Even the quadratic formula used to check the equation also result in normal value

Fig 8. Checking with quadratic formula

I just wanna ask, is there something wrong with the equation or the value that substituted into the equation? Thanks for reading all of this.


r/AerospaceEngineering • • 1d ago

Other can the plane gain lift while being stationary?

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534 Upvotes

r/AerospaceEngineering • • 7h ago

Discussion Inquiry regarding CFD simulation for high-pressure fluid dynamics

2 Upvotes

am an independent researcher exploring high-pressure supersonic closed-loop fluid dynamics. I am looking to connect with a simulation expert who has access to CFD tools to discuss and test a kinetic-to-electrical energy conversion module under strict confidentiality. If anyone is interested, please DM me.


r/AerospaceEngineering • • 15h ago

Discussion What application actually justifies an air/ground transforming drone? Feeling stuck on my thesis

8 Upvotes

I'm building a transforming drone inspired by the M4 morphobot for my project, but simplified to just two modes: flight and ground mode. I know the main argument for adding ground mode is power saving. In the M4 paper, their robot consumed 3000W in flight mode but only 30W driving on the ground which is a huge 100x difference if you need to stay deployed longer or navigate indoor spaces.

The issue is I'm still really struggling to find a solid real-world application that justifies the trade-off. The morphing mechanism adds a ton of weight and mechanical complexity, which hurts flight time. Plus, ground mode is super slow. It feels like in 99% of cases, you'd be better off using a regular drone or a cheap rover. What kind of application would actually justify this design? Like a scenario where a pure drone fails AND a pure rover fails, so a hybrid is strictly required?

I've pretty much run out of ideas and I'm starting to feel like I'm building a gimmick looking for a problem. Am I cooked or is there a legit use case here?


r/AerospaceEngineering • • 3h ago

Discussion Are pvc rocket motor save?

0 Upvotes

Thats the question thats all just with kraft paper liner. And please recommend how to make the nozzle.


r/AerospaceEngineering • • 21h ago

Personal Projects Updated simulation of an oscillatory aircraft based on my experiments. Now it's bionic.

10 Upvotes

I have refined the aeroacoustic/vibration-based aircraft simulation that I posted previously:

https://www.reddit.com/r/AerospaceEngineering/comments/1tqoq9m/oscillatory_propulsion_simulation_and_simple/

It is now more versatile, featuring both "jellyfish" and "fish" modes. The underlying principle remains the same: the fluid does not act directly on the craft's surfaces; instead, the forces derived from the fluid are converted into thrust via an accumulator. However, thrust is no longer generated simply as a phase-shifted inversion of drag. Rather, energy is captured from low-pressure regions—stored as potential energy—and then released through a "collapse" mechanism, with dynamically evaluated recovery and shock coefficients.

This approach yields a more realistic relationship between propulsion efficiency and parameters such as frequency and amplitude, expressed via Strouhal numbers. The feedback loop between internal oscillations and drag acts as an automatic frequency-tuning mechanism.

Additionally, the model incorporates simplified lift and drag forces acting perpendicular to the thrust vector.

The code can be found here:

https://github.com/MasterOgon/Aeroacoustic-Flying-Saucer-Oscillating-Resonator-CFD-Simulation-LBM-/blob/main/README.md


r/AerospaceEngineering • • 20h ago

Discussion Maintainability in Spacecraft vs Aircraft

4 Upvotes

I am an A&P mechanic and always wonder why engineers design stuff the way they, especially when it makes my job incredibly difficult. I understand there are outside factors, like the engineer wanted it one way to make it easier to access, but budget or bosses won’t allow it. I’m not complaining about that at all.

My question is, are spacecraft designed with LESS maintainability since their tolerances are even tighter than aircraft? Looking for any input on the subject, I’m genuinely curious.

TLDR: Are spacecraft even more of a pain in the ass to work on than planes?


r/AerospaceEngineering • • 22h ago

Personal Projects RC plane question

4 Upvotes

Hi, engineers. I hope this is the right place to ask this.

My son is an MS student in AE, and he has requested an RC plane kit for Christmas. He has built a couple of RC planes with a club and designed and built an airplane for AIAA, but I wouldn’t say he’s had a ton of experience compared to hobbyists.

I know nothing about RC planes. Does anyone have a brand or company they recommend? Is keeping it under $200 pretty reasonable? Any kits you particularly enjoyed building and flying? Thanks!


r/AerospaceEngineering • • 21h ago

Discussion Will a estes sized rocket motor be able to make a rc plane take off?

0 Upvotes

A question thats been in my mind for a few days. I wondered if it is powerful and long enough to make it take off. Taking off like a plane not a rocket tho so it will be a glider after take off.


r/AerospaceEngineering • • 2d ago

Career 217 aerospace engineering internships and new grad jobs open now (Blue Origin, Northrop Grumman, SpaceX, RTX, Relativity Space), free lists

96 Upvotes

aerospace internships are spread across a lot of separate company career pages, so i pulled the ones open right now into free lists, straight from employers' own job boards. no sign-up, it's all on github:

  • aerospace engineering internships and co-ops (50): https://github.com/mehek-builds/Aerospace-Engineering-Internships
    • 50 at 17 US employers (Blue Origin, Northrop Grumman, RTX, Ursa Major, Axiom Space, Sierra Nevada Corporation, AeroVironment, The Aerospace Corporation)
    • 32 propulsion, avionics, GNC and flight test, 9 spacecraft, aircraft and aerodynamics, 10 general aerospace
    • 22 posted in the last week, 7 at employers with a visa sponsorship record
  • new grad and entry level mechanical, manufacturing and design engineering (167): https://github.com/mehek-builds/Mechanical-Manufacturing-Design-New-Grad-Jobs
    • 49 at aerospace and space employers (Northrop Grumman, SpaceX, Relativity Space, Sierra Space, Boeing, RTX)

posting date on every row, rebuilt every monday.

comment which area you're looking for (propulsion, GNC, structures, new grad) and i'll send you a list for it.


r/AerospaceEngineering • • 2d ago

Discussion What kind of fuel can be used in hybrid rocket motor?

4 Upvotes

Just a question but the answer is probably no. Can sorbitol and red iron oxide be used like solid motor?


r/AerospaceEngineering • • 2d ago

Personal Projects What it took to get my 249g 3D-printed V-tail FPV wing flying exactly how I wanted

89 Upvotes

Building on my experience designing tailless flying wings, I wanted to explore a more complex configuration with a closely coupled V-tail.

Not complexity for its own sake, but an opportunity to better understand how different aircraft systems interact.

Different wing geometries. Different tail configurations. Different propulsion systems.

I used OpenVSP and VSPAERO to investigate the aircraft's aerodynamic characteristics and stability, then developed the geometry in Onshape before moving into prototyping and flight testing.

The original design used four tractor motors, but flight testing revealed some interesting challenges.

The four-motor arrangement introduced strong throttle-to-pitch coupling, producing a significant nose-up pitching response under power. Without that contribution from the propulsion system, the aircraft was noticeably pitch-stiff, with insufficient control authority for the manoeuvrability I was looking for.

This led me to explore different propulsion arrangements, CG positions and control configurations, eventually moving to two larger motors and distributing pitch control between the wing elevons and V-tail ruddervators.

The final arrangement uses the elevons for both pitch and roll, while the ruddervators provide pitch and yaw control.

It's not necessarily an optimal solution from an aerodynamic or control perspective, but it has proven highly functional in flight, giving me the manoeuvrability and control response I was looking for.

One area I'd like to investigate further in future iterations is the use of independently actuated, all-moving V-tail surfaces in similarly close-coupled configurations.

Final specifications:

  • Wingspan: 600mm
  • Flying weight: 249g
  • Configuration: Twin tractor, closely coupled V-tail
  • Propulsion: 2× 1103 brushless motors
  • Battery: 2S 1000mAh LiHV
  • Flight controller: Matek F405-Wing WMO / INAV
  • FPV: DJI O4 Wide
  • Construction: 3D-printed colorFabb LW-PLA
  • Flight time: Approximately 7–9 minutes

Some experiments worked. Others challenged my assumptions, sometimes the hard way!

But with every iteration, my understanding improved, and the aircraft gradually converged on the flight characteristics I was looking for.

VENOM now flies exactly how I intended (damn beautifully), and I'm really happy with how the project turned out.

On to the next challenge!

More info on VENOM


r/AerospaceEngineering • • 2d ago

Cool Stuff NASA Experimental Mars Helicopter Blade Designs Target Longer Flights

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15 Upvotes

r/AerospaceEngineering • • 1d ago

Personal Projects Hey guys do you maybe know where to find dat files for kfm airfoils?

1 Upvotes

I want to use kfm airfoil in my project and I'd like to run some simulations but I can't find any .dat files or geometry desciptions that would help me to draw one. Do you know any database I can try?

Thanks.


r/AerospaceEngineering • • 2d ago

Career Best Books and Resources to Learn GNC from Scratch in One Month

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1 Upvotes

r/AerospaceEngineering • • 2d ago

Personal Projects Flight computer for a VTVL rocket

1 Upvotes

Hi everyone

We’re prototyping a VTVL rocket with a target altitude of around 3,000 m. We’re currently working on the PCB design and deciding on our flight control architecture.
We’re considering three approaches:

1-Adapting and improving an existing open-source rocket flight computer

2-Designing our own hardware and firmware from scratch.

3-Using a Pixhawk as the flight controller, with a separate onboard computer handling telemetry and communication with the ground station.

Which approach would you recommend for this kind of project? Would a separate computer for communications be useful, or would it add unnecessary complexity?
We’d appreciate any advice, relevant open source projects, or experience using Pixhawk for VTVL applications.


r/AerospaceEngineering • • 3d ago

Other Will we ever develop electric airplanes for commercial travel?

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0 Upvotes

r/AerospaceEngineering • • 3d ago

Discussion Is it possible to turn a solid rocket motor into a hybrid rocket motor?

0 Upvotes

Its a concept idea ive thought of and possibly someone already did it. If i keep the casing and the nozzle but change the bulkhead into being able to connect with the oxidizer tank will it work? But yes we would need to control the thrust so the nozzle can withstand it without exploding into our faces.


r/AerospaceEngineering • • 3d ago

Career Looking For a Co-Founder!!!!!

0 Upvotes

Hey everyone! I'm a final-year CSE student from Bengaluru, and I've
been thinking about an idea in the deep tech defense space for a long
time. I'm keeping the details private for now, but I'm very passionate
about it and ready to put in the work. I'm looking for a co-founder
who is in their final year or has just graduated, comes from an
aerospace background or has already worked in the field (internships,
projects or research), and is genuinely passionate about startups. We
can research, validate and build this together, and grow the team as
we go. If this sounds like you, Please DM me .


r/AerospaceEngineering • • 3d ago

Discussion Tips on networking

1 Upvotes

Id love tips on networking! im an high school student and am hoping to get into the aviation or aerospace industry and the first step would obviously be a good degree in Mech E or Aero E. So meeting any good friends or mentors or anyone who can help and talk me along the way would be appreciated :)


r/AerospaceEngineering • • 4d ago

Discussion What's the future of CFD in aerospace? Will open-source eventually take over?

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5 Upvotes

r/AerospaceEngineering • • 4d ago

Discussion What the hell do you guys do with all your patches

16 Upvotes

What do you guys (space/aero professionals, academics, students) do with all your mission/project/event/org patches? I've been amassing quite the collection in only a few years in the industry and I'm not quite sure how to best store/display them.

I don't really want to apply them on clothes I would wear outside of work, and while I thought I could get a specific jacket/vest for all of them I would quickly end up looking like these guys.

I think they're a fun way to show off the cool stuff you've been involved with throughout your career, it would be a shame for them to just collect dust in a drawer.


r/AerospaceEngineering • • 5d ago

Media would you rather buy a gyroplane or raise a child

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502 Upvotes