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Questions tagged [aerospace-engineering]

Aerospace engineering is the primary branch of engineering concerned with the research, design, development, construction, and testing of aircraft and spacecraft.

1 vote
2 answers
24 views

Assuming sufficient electrical power, is an electrolysed oxyhydrogen rocket practical?

Assume we have access to light electrical power e.g. a (hypothetical) small fusion reactor. Is it practical to operate a water-fuelled rocket, in which water is converted to hydrogen and oxygen (or ...
Louise's user avatar
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0 votes
0 answers
15 views

How do I learn about Rockets and planes?

I want to learn how to make aeroplanes and rocket, how they work, etc. I want to be able to make working models. How do I go about it, what books can i read, what videos can I watch for easy, clear ...
Sriansh's user avatar
0 votes
0 answers
7 views

How could predict the affect the of adding another element to alloy in the terms of thermal conductivity and material wear resistance?

I'm interested in the effect thermal conductivity affect and material wear resistance by adding different element to an already high thermal conductivity like GRCop-42. My main interest are to the ...
Isaac Francis NSR Rutherford M's user avatar
-3 votes
0 answers
35 views

Deriving the longitudinal equations of motion for an aircraft

I'm trying to create a state-space model for the pitch control of an aircraft as described here: https://ctms.engin.umich.edu/CTMS/index.php?example=AircraftPitch&section=SystemModeling The ...
HonHonHon's user avatar
0 votes
1 answer
29 views

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 ...
Aerospace_Nerd's user avatar
0 votes
1 answer
21 views

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 ...
Bogdan's user avatar
  • 3
0 votes
1 answer
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High-level sun sensor modelling for satellite

I am searching for some references on how to model at high level a sensor in terms of the statistical interpretation of the errors (bias, noise, ecc). Do someone have any reference (books or papers) ...
daniele__'s user avatar
0 votes
0 answers
25 views

I'm Missing Something on Problem 3 in Section A5.4 of Bruhn's Analysis and Design of Airplane Structures

I've been working through the 1943 edition of Bruhn's Analysis and Design of Airplane Structures. I found an archive.org pdf version of the 1948 edition that includes answers to select problems, as ...
brandonman's user avatar
0 votes
0 answers
32 views

Is front shroud more thick than the lower shroud used in impellers ? Thickness of shrouds of shrouded impellers used in turbo pumps of rocket engines

This is an impeller used in turbopumps for increasing the pressure of propellants to drive the rocket engines. I wanted to ask all the engineers currently working in manufacturing of these impellers ...
Lakshay's user avatar
1 vote
1 answer
48 views

Why do wing-tip vortices cause an induced angle of attack upstream?

My question is the following. Wing-tip vortices induce a downward flow on the root side of the wing. So, if this induction happens at the wing, and these vortices are then shed downstream, why is ...
Armaan Mohammed's user avatar
0 votes
1 answer
45 views

Why do trailing edge flaps increase the CL,max of a wing?

I was wondering why do trailing edge flaps increase the lift co-efficient for a given angle of attack. I am guessing it has something to do with delayed flow separation, but this is quite unintuitive, ...
Armaan Mohammed's user avatar
0 votes
0 answers
27 views

CubeSat: When designing the PID Controller of the CubeSat, what are some constraints that you need to take into account?

For a 1U CubeSat project in which we need to design the controller for it. We decided to not include any propulsion system to keep it light, we'll just essentially drop the satellite on LEO and let it ...
tadm123's user avatar
  • 103
0 votes
2 answers
109 views

Wind Load on conical structure

Is there a way to calculate the wind load acting on this conical cylinder? The wind pressure blowing through the hollow conical cylinder is at 30 bar. The conical cylinder is tilted at 10 degree ...
Matt's user avatar
  • 1
0 votes
0 answers
51 views

How to modify a ball valve to make it cryogenic

I have designed a manual non-cryogenic ball valve in SolidWorks (based on this tutorial: https://www.youtube.com/watch?v=pYsU1gfx-00) My aim is to modify this CAD design so that it becomes cryogenic (...
user71318's user avatar
0 votes
0 answers
35 views

Fuel cell power output

I've spent innumerable time over the years looking for commercially available hydrogen / oxygen fuel cells that might actually be usable in one project concept or another. The best I've ever managed ...
Slartibartfast's user avatar
0 votes
1 answer
83 views

How would I do stress analysis on a fuselage like this?

This is a frame for an RC plane that I have designed using balsa wood and prefabricated carbon fiber flat bars. It will have a balsa wood skin on the outside, but I have yet to figure out how to ...
bens's user avatar
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0 votes
1 answer
39 views

When something undergoes angular acceleration (like a bar) how does the distribution of forces look along the bar?

This is something kind of explained with propellers and turbine blades but I'd love some good explanations. Thank you!
Mechs_and_Specs's user avatar
0 votes
2 answers
228 views

How does stalled diffuser/wing reduce drag at F1 car?

How stalled diffuser/wing reduce drag at F1 car if in aerodynamics stall/separation is always related to increase in drag? Any graph of pressure distribution when diffuser is stalled? From "...
22flower's user avatar
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0 votes
0 answers
40 views

In orbit rocket launch

If fuel is sent into space in bulk using space station as a "Fuel Depot", then how fast and efficient could in orbit launches of objects like probes, etc be? Rockets use huge amounts of fuel ...
LazyReader's user avatar
2 votes
2 answers
85 views

Helical inserts on aerospace parts work intermittently

I work at a machine shop with high-volume parts and a lot of threaded holes. Common sizes are 1/4-28 STI and 10-32 STI. Every hole gets a helical insert. We have always had major issues with the 1/4-...
Woody's user avatar
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8 votes
6 answers
5k views

Can we add treadmill-like structures over the airplane surfaces to reduce friction, decrease drag and producing energy?

I am curious about a method to enhance the efficiency of passenger aircraft during cruise speeds by integrating treadmill-like structures on the fuselage and beneath the wings without changing the ...
Siames's user avatar
  • 81
1 vote
1 answer
74 views

Jitter Experienced by Spacecraft from Reaction Wheel Imbalances

I am working on a project trying to model a satellite's pointing error caused by jitter from the reaction wheels. I have found a couple of papers (Paper 1 and Paper 2) which implement the simple model ...
Sam's user avatar
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0 votes
0 answers
20 views

How to estimate air velocity at turbine in turbojet?

I am designing a small turbojet. I wanted to know how to calculate the air volume expansion to predict the outlet velocity of air towards the turbine. Theoretically, I wouldn't know the flame ...
user43461's user avatar
0 votes
2 answers
67 views

Can we use ion thrusters in space to relieve tension on a space elevator cable?

I suspect/hope I'm not kidding myself too much with the physics of this; it seems to stack up in my mind; but can we not relieve tension on, say, a steel cable running from a space station in orbit ...
Sam Cottle's user avatar
-1 votes
1 answer
62 views

Atomic weapon design book [closed]

I’m starting my degree in nuclear engineering in September and was wondering if anyone knew any good books for Atomic Weapon design please?
Jamie's user avatar
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1 vote
1 answer
34 views

Is there a way to 'switch OR engage/disengage' power between two different rotating shafts depending on a set RPM (wind speed)?

I'm a final year mechanical eng student, I'm working on designing a prototype of a 'Hybrid vertical axis wind turbine (VAWT)". This hybrid turbine consists of two types of VAWTs Savonius & ...
Yashwanth SriHari's user avatar
-2 votes
2 answers
67 views

Is there a table for the density, Young's modulus, and other common properties for the most common materials?

I've tried googling extensively, but I have not found a single table that contains many of the "common" materials and more than one property. Does anyone have a table from an engineering ...
giuli0110's user avatar
0 votes
0 answers
49 views

Help relating thrust to angular velocity of helicopter in hover

Given a system consisting of an engine and propeller, I want to determine the maximum thrust it will produce when in stationary hover (no forward velocity) above the ground, and what angular velocity ...
Jacob's user avatar
  • 1
0 votes
0 answers
17 views

What is the optimal weight ratio for a multistage water rocket?

I do know about the Tsiolkovsky rocket equation for optimising multistage rockets, however the equation requires a fixed exhaust velocity which is something that water rockets don't have, so for this ...
notanengineer's user avatar
1 vote
1 answer
79 views

Optimizing Launch to LEO

I recently decided I would try to develop my own launch to LEO optimizer, as I have always been fascinated with the complexity of that problem. I have been using matlab, as I am very comfortable with ...
Frank's user avatar
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