I have a problem which I cannot crack, I am currently looking into the use of a universal joints but I want to explorer other routes too.
I am working on a gearbox test rig which requires a means of transmitting a thrust (5000 N), a torque (1800 Nm) and a speed (2000 RPM) all in the same...
Hi guys,
I need to be able to estimate the thrust that a turboprop propeller produces at sea level static. Say I have an 1100 hp pt6a engine and a 80 percent efficient propeller. I have seen formulas that calculate the thrust but you need to be moving. I want to know the static (your airplane...
Hello everyone this is the biggest engine i have ever made. You could see at the end i ran away leaving the cylinder and the camera woman ran away. Really i didnt expect so much sound. Used one pair of injectors and fueled only two intakes.
Actually i closed one of the intakes because my tank...
Hi,
I'm wanting to do a fun numeracy exercise for my students. I'm planning to have them construct bottle rockets, take measurements and then calculate/graph how high their rockets get using simple triangulation. From that, I was hoping to get them to calculate what the thrust was of their...
I wanted to use a disco ball motor to rotate an object weighing approximately 125lbs. The motor was rated for 25 lbs. Motors rated for higher weights had much higher costs, beyond what would be practical.
It was suggested that using an arrangment like the one described in the attached pdf would...
Does anybody know some ballpark figures for thrust to power, Newtons per watt, ratios for modern propulsion systems, mechanical drive train ie cars trucks, propeller driven craft, boats planes, and rockets.
I've found one reference that states the F/P ratio for a DC-9 jet engine is 0.016 N /...
Homework Statement
i built a boat for physics class with an electric motor. we are asked to calculate the thrust of the motor and the resistance of the hull using Newton's second law of motion. i conducted an experiment (to collect data in order to find resistance) that required a string...
Hello all,
Just wondering if anyone can give me some guidance on this: the problem is an apparent contradiction I've stumbled upon. Some sources (e.g. www.braeunig.us) suggest that maximum thrust is achieved when Pe=Pamb (i.e. exhaust pressure = ambient pressure)l whereas others say that...
Hi
I have been trying to figure out the force experienced by individual components of a gas turbine engine.
Generally, the thrust of the engine is defined / calculated as the change in the momentum of the fluid. Usual formula is mass flow X (C_jet - C_intake) + the pressure difference in...
Hi there -
I built a small electronic turntable with the following components: 1- Arduino 2- Sparkfun easy stepper driver 3- Stepper motor 4- Servocity set screw hub. 5- Thrust bearing from mcmaster-carr (square turntable, found here http://www.mcmaster.com/#swivel-plates/=eltxix) 6-...
I need some information and guidance on how to calculate net lift and thrust produced by wings of an MAV(micro air vehicle) which are flapping and active pitching.
I know only about one method which is the Blade Element Analysis, but it is just an approximation and doesn't accounts for...
Thrust and Mass verses g force upon object
Have designed a solid fuel and liqiud fueled rocket engine.
Not great in mathmatics!
Have total weight of fuel engine and power supply at 2.3 pounds
Have an engine that burns for 3.3 seconds and produces 47 pounds thrust for 2.1 seconds.
If I...
Hi I am building a quadro-copter, and I'm curious to know how i can calculate the thrust generated by a motor/propeller combo. The motors are brushless electric motors for which i know the max RPM. The propellers are two bladed for which the diameter and pitch are known. Is there a simple...
Homework Statement
[PLAIN]http://img714.imageshack.us/img714/8184/rocketj.png
I am not sure if the problem has enough information to find. However, i tried some of the works.
g=10m/s2( i use gravity as 10 .)
Homework Equations
No idea...
The Attempt at a Solution
I am...
I want to make a quad rotor UAV. i studied a lot but i did not find how static thrust is being calculated. In physics forum i have found an equation which is given below but i can not understand what is 'frac' and 'rho'.
Equation is:
T=\frac{c_T}{c_p}\frac{P}{nD}
Where:
P = power (ft-lb/s...
I'm a math guy taking engineering classes more or less for fun, so some of the stuff I should know I probably missed in a basic dynamics class. I feel really dumb that I can't figure this out.
I'm in a vehicle dynamics class and I have to calculate the constant thrust T for the following...
For example then talking about the rocket the trust is:
F_thrust = u*dm/dt
where u is speed of the gases relative to the rocket, and dm/dt rate of change of ejected mass of gases.
Now if the rocket is being launched vertically so force of gravity acts upon it and:
F_net = F_thrust -...
First of all this is not a perpetual motion machine and is not the previous U Reusable Fuel Transit Drive I designed earlier. This type of transit drive, which doesn't reuse fuel, works in theory by having two combustion chambers and their respective exhaust nozzles positioned parallel to the...
Is there any Advanced concepts , theories out there; Instead of the combustion. We're not limited ; direct conversion of electricity to thrust is here, so if you have any ideas leave it here,
*Electricity-conversion- microwave- to thrust (radiation pressure difference)
*Electricity-conversion-...
Horizontal water rocket thrust calculations - HELP!
Hi All,
I want to accelerate a 90kg body at a rate of 2 m/s2 for a period of 1 second using thrust developed from a number of water bottle rocket jets. Based on the drag coeff calculated I believe I need to develop 190N of force.
A...
Disclaimer: I'm not a physicist nor do I know calculus, but I'd appreciate a little guidance with a concept I've been thinking about. I know one would usually pay for this kind of advice, but since it's just for entertainment, I'm not asking for any equations to be solved, unless you're in the...
first off, thanks to any that respond w useful info :)
the end answer i need to find on the first topic is how many atoms of hydrogen are required to propel a mass of "x" at an acceleration of 1g in space (assuming no gravitic influence) but i would settle for how to figure out what the fuel...
Homework Statement
I would like to be able to calculate the energy use per second, to maintain a rocket of given mass, at zero velocity, i.e. hovering, at, say, sea level.
Homework Equations
I have Thrust = Force times velocity, but can't work out the energy due to the velocity of the...
Dear native English-speaking professionals!
I am making up an info table concerning railcar operating loads, and I’m a bit stuck with one term - I’m not sure if it sounds comprehensible enough to an Enflish speaking reader.
Here is the part I’m struggling over:
"Load description: cargo...
Can sound from any source create thrust??
hi there,
since I'm new to this forum, i don't know whether this the place to put up a question like this...!
if I'm wrong my sincere apologies
let me head to the topic now...
i wanted to whether the sound waves created form any source can...
Hey guys! I'm new to the forums here and was after some help for something that I am currently working on. I need help converting cfm to thrust, i have found the formula though i can't get my head around it.
Here it is:
CFM = Cubic Feet per Minute = Volumetric Flow Rate
Mass Flow Rate =...
Hi! I have a question about how thrust is made from a turbojet engine.
The most common explanation goes something like "As the fluid gets accelerated there is a net force". I don't think this explanation is either good nor rigorous.
The force that accelerates the fluid is, of course, the...
Homework Statement
Sam, whose mass is 71.0 kg , takes off down a 51.0 m high, 11.0 degree slope on his jet-powered skis. The skis have a thrust of 210 N . Sam's speed at the bottom is 41.0 m/s .
Homework Equations
I'm not sure which equation(s) to use.
Net Force= ma and some kinematic...
I finally figured out what my previous problem was in my last question posted. I have obtained the plots required but I am a little confused about the trends.
(1) At low Mach, should my thrust be lower compared to the value at a higher Mach?
(2) Should the RPM decrease with an increase in...
hello
a plane would need a thrust to weight ratio of 1 of fly straight up without losing speed
but how can a plane in level flight maintain its altitude with <1 TWR
since to maintain a level flight you need to have lift = weight
so your engine needs to supply enough power to generate...
Imagine there are 2 space-probes in space. Both of them start their engines in the same time. The first space-probe has a very low level of thrust but a very high specific impulse. The second space probe has a very high thrust but a very low specific impulse.
Both of them have an equal amount...
This is not my homework this is just a random thought. Say you have a 1 kg helicopter hovering in midair. The question is, given perfect efficiency, how much power is it using to hover?
My approach is to think of the given information first. We know that g= 9.8. So you have a 1 kg mass that...
hello guys iam ganesh..iam a mechanical engg student and iam new to this forum and this is my first post here..
these plans are uploaded by eric and technical help given by metiz..take a look at it..
I posted I question in regards to shock angles on this very same problem earlier but now I have a new problem. I need to calculate the heat rate required in the combuster in order to ensure that the vehicle will cruise (delta z=0). I also need to find the mass flow rate of the fuel. h for the...
Sorry; this is like soooooooo hard
Homework Statement
A car with a mass of 1500 kg has en engine which can produce 4000N of thrust. Assume that the air resistance on the car is a constant 500N. If the car starts from rest, how fast will it be moving after 10 seconds.
Homework Equations...
Can anyone help me?
I'm doing a question on aircraft propulsion technology and I'm stuck.
The question is:
'If the mass of air through a propeller is 1000 Kg/s, the aircraft's velocity is 100 m/s and the slipstream velocity is 120 m/s, calculate the thrust?
Attempt at answer...
Homework Statement
What is the average acceleration until burnout of a spacecraft engine creating 53.2MN of thrust with a propellant velocity of 4.78km/s? The initial mass is 2.12x10^6 kg and final ,*** is 7.04x10^4.
Homework Equations
0 = m(subscript_f)v(_f) + m(_r)v(_r)
The...
Hi everyone, as you can tell from the title, I'm having some trouble understanding thrust. Here's what my textbook says:
"m(dv/dt) = -u(dm/dt) [where u is the speed of the exhaust relative to the rocket and dm/dt is negative]
Now dv/dt is the acceleration of the rocket, so the left side of...
Homework Statement
I need to find required thrust power for lockeed s3a. I know Thrust=Drag in horizontal flight.
For take off, need to use the take off angle, split the Weight (G) into 2 components using the takeoff angle... Same for landing.
Given:
G=19278kg ---> 19278*9.81=189,1kN...
Homework Statement
A polaris missile has a mass of 1.4 x 10^4 kg and its engine has a thrust of 2 x 10^5 N. If its engines fire in the vertical direction for 1 min starting from rest, to what vertical height would it rise in the absence of air resistance?
Homework Equations
F=ma
W=mg...
If a rocket doubles it's relative exhaust velocity while do tripling the "burn rate" of fuel, the thrust...
A) doubles
B) Triples
C) increases 5 times
D) increases 6 times
E) none of the above!
Thrust=dv/dt=lVe(dM/dt)l
I just plugged in 2 for V and 3 for dM and 1 for dt giving me 6
Homework Statement
The idling engines of a landing turbojet produce forward thrust when operating in a normal manner, but they can produce reverse thrust if the jet is properly deflected. Suppose that while the aircraft rolls down the runway at 150 km/h, the idling engine consumes air at 50...
1. A solid bar of length L = 0.5m and with W = 0.1m weighs 2kg. It also has two constant-thrust rockets attached on either end. Each rocket is small enough to be considered a point mass of 0.25kg. If the bar is initially at rest and in two seconds after the rockets are fired it achieves a...
Greetings,
I want build an interstellar probe.
Given the power of the laser beam and the mass of a mirrored object a laser is shining on, how does one calculate the thrust or acceleration?
Thanks
Homework Statement
The first stage of a Saturn V space vehicle
consumes fuel at the rate of 47400 kg/s, with
an exhaust speed of 2820 m/s.
The acceleration of gravity is 9.8 m/s2 .
Calculate the thrust produced by these en-
gines.
Answer in units of N.
(part 2 of 2) 10.0 points
Note...
Hey guys, I'm a college student looking to build a miniature RC plane based off this picture here: [PLAIN]http://www.kruxor.com/wp-content/uploads/2010/07/SC2_Banshee_Art.jpg
As you can see, the thrust needed to lift and mobilize the plane is provided by the two fans on the sides (does this...
Hello,
I was trying to find out why net thrust decreases then increases with velocity. I recall there is pressure and momentum thrust, however I can not recall why one of them falls away and the other increases.
Is momentum thrust the one that picks up as the mass flow increases with...
Homework Statement
The 3rd and 4th stages of a rocket, mass 40kg and 60kg respectively, coast in space with a velocity of 15,000kmh when the 4th stage ignites, with thrust T and causes separation. If the velocity of the 4th stage is 10m/s greater than the 3rd stage at the end of the 0.5...