An aircraft is a vehicle or machine that is able to fly by gaining support from the air. It counters the force of gravity by using either static lift or by using the dynamic lift of an airfoil, or in a few cases the downward thrust from jet engines. Common examples of aircraft include airplanes, helicopters, airships (including blimps), gliders, paramotors, and hot air balloons.The human activity that surrounds aircraft is called aviation. The science of aviation, including designing and building aircraft, is called aeronautics. Crewed aircraft are flown by an onboard pilot, but unmanned aerial vehicles may be remotely controlled or self-controlled by onboard computers. Aircraft may be classified by different criteria, such as lift type, aircraft propulsion, usage and others.
Well Last week I was on a website called the biplane forum. I posted a topic about a very serious real world problem. I own a pitts S1S aircraft. This aircraft is an experimental aircraft. Not certified. Pitts are very popular airplanes in the aerobatic world. There are many different models...
I need help finding the forces when an aircraft’s jump cable catches to stop a plane on an aircraft carrier ship. The aircraft is traveling at 110 mph with the front of the plane 3 feet off the deck of the ship. If the assumption is made that the cable stops the aircraft immediately (the cable...
Homework Statement
An aircraft is landing on a carrier ship in the middle of the Pacific. When the aircraft’s jump cable catches to stop the plane, the aircraft is traveling at 110 mph with the front of the plane 3 feet off the deck of the ship. If the assumption is made that the cable...
doesn't the aircraft leave its track through satellite?
i mean why they are unable to locate aircraft lost in sea like airfrace flight 447
if the whole track of an aircraft is known, wouldn't the exact position where it lost contact with the satellite be known then and no need of an ELT...
Here's what I know from basic tech school: Flaps = trailing dge and slats = leading edge. ?Flaps and slats aid in both take-off and landing. I'm just not sure how they do so. My guess is that during takeoff, the combo increases the wing surface area thus allowing lift at lower airspeeds...
Hi, I don't know how hard this problem really is, I've tried setting up a differential equation and get garbage answers. Can anyone help me?
Imagine two identical aircraft with identical drag, wing area and thrust but different payloads, such that one has a max straight and level speed of...
Hello people. I've been making a sim of a P-51 Mustang in Blender3d and am working on the physics. I've got the Drag, Lift and Thrust with help from here. I need help now with:
Flight Dynamics (Roll, Yaw and Pitch physics)
I need to know the amount of force regarding torque on the aircraft...
I have this problem and it seems like it has a simple solution, however I can't seem to figure it out.
Using the following values and the previous equation calculate the rate of climb for a
typical airplane at an altitude of 8000m.
4 Engines each with 150kN of thrust.
Aircraft mass is...
Homework Statement
An aircraft has a lift-off speed of 40m/s. How long does it take the aircraft to be airborn after a takeoff run of 320m?
Homework Equations
I know that I have to divide 320m by the speed (40m/s). But if I do that, I get a wrong result. The result should be 16s and this...
As the title states, has there ever been an aircraft, that has never crashed?
Just for clarification, I mean a TYPE/MODEL of aircraft (for example Boeing 757) not a specific aircraft. So please, no random aircraft registrations of currently operating aircraft!
Jared
I will soon be starting to design either a transonic or hypersonic military aircraft.
I'm just curious what software would be best to use, I have previous experience with MatLab and AAA (darcorp).
I'm not sure if AAA will be able to work correctly at those speeds.
Any help would be great...
So I know that the faster the fluid moves the lower the pressure . But what I don’t get about an airplane wing producing lift , so the plane is cutting through the air , and the air molecules are still . Why does the air molecule on the top part magically just speed up ?.
Hi, I hope someone can help me with this question, I originally posted this question in the homework help forumbut no one seems to be able to help me with it. I think my problem is more math related - I don't really know where to start.
I have been a given a matrix containing aircraft...
Hi, I hope someone can help me with this question, although its aeronautical engineering, I think I have more of a maths related problem - I don't really know where to start.
I have been a given a matrix containing aircraft equations of motion (see attached picture). Also shown is an equation...
Hi
For an initial approximate, I am modelling an aicraft wing as a cantilevered beam. I want to model the beam to incorporate the different materials used; a composite plate is sandwiched between a foam material and therefore the stiffnesses are different. How can I take this into account or...
Hello All,
My first post here - I wonder if anyone can help?
I am attempting to apply fracture mechanics to an investigation of an aircraft structural component, and am having difficulty finding a suitable method of adequately calculating the total applied stress (hence 'landing...
Hi, I am trying to work out the ground run distance of takeoff for an aircraft. I can't really write the formula down because of the length and many variations of it so I am just hoping that you know what I am talking about.
I am trying to work it out for a cessna 172 so i am expecting a...
I'm trying to figure out the average deceleration of an aircraft that touches the ground at 104 knots (175.53 ft/sec) and decelerates to zero in 3200 feet? Does anyone know how to do this? Thank you very much to all who reply.
Hi,
I need to make changes to an existing design of a model radio controlled aircraft to increase its lift to carry more payload. Pls confirm my ideas and any suggesstions would be really appreciated.
Using wingtips to reduce induced drag and increase lift.
Will a Dihedral affect lift in...
I have 2 questions.
Homework Statement
1)An aircraft is flying at sea level at a speed of 280km/h. Calculate the static pressure and total pressure at the stagnation point. From a standard atmosphere table, for sea level altitude, pressure is 101325 Pa. Density of air is 1.2250 kg/m3.
2)...
Though I'd scan for ease ;)
Homework Statement
Check the Pendulum question out http://dl.getdropbox.com/u/37461/physhelp/secC1.png and http://dl.getdropbox.com/u/37461/physhelp/secC2.png,and the http://dl.getdropbox.com/u/37461/physhelp/secB1.png.Homework Equations
Should all be in the...
I'm trying to solve a problem which involves the following scenario. Any help would be great!
A landing aircraft (mass 14 tonnes) is to be slowed from 300km/hr to 180km/hr in 3 seconds, by the deployment of two identical parachutes at its rear. Determine the diameter of each parachute. The...
momentum transfer?
when aircraft is in motion, it has momentum.
Since it has momentum, there is momentum transfer taking place between the aircraft and the air particles. During this momentum transfer what exactly is happening between the wings and fluid particles that are present right...
Homework Statement
As an aircraft approaches landing, the components of its position are given by:
x=81t y=500-27t
Velocity vector of aircraft during descent is given by:
81m/s (i hat) + -27m/s (j hat)
The value of the speed during the descent is:
85.381m/s
What angle does the velocity...
Homework Statement
An Airbus A320 jetliner has a takeoff mass of 75,000 kg. It reaches its takeoff speed of 82 m/s in 35s.
Find the Thrust of the engines, don't worry about air resistance, but rolling friction is substantial.
Homework Equations
Fnet=mass*acceleration
a=(82/35)...
Heard on the radio that the aircraft that crash landed at London airport crashed because of ice in the fuel (or that is the best guess) surly this is a cop out.
An aircraft flying in a straight line at constant height h and speed U drops a package
on a target at ground level. The package is subject to air resistance whose magnitude
is kmv where v is the speed of the falling package, m its mass, and k > 0 a constant.
(a) Show that the vertical...
Homework Statement
4) The wing of an aircraft is 60m long and the aircraft is traveling at 250ms-1. The vertical component of the Earth’s magnetic field, which the wing is cutting, has the value of 4.3 X 10-5 T.
Calculate:
a. The Flux cut per second by the wing
b. The induced emf set up...
Homework Statement
A jet aircrft climbs in a straight line at an atitude of 60 degrees to the horizontal the jet thrust amounts to 90 kn the mass of the aircraft is 8 tonne and the average air resistance amounts to 11kN calculate the time taken to reach a height of 3km if the speed at the...
This is what I understand about Kelvin's Circulation Theorem
1)for inviscid (where the viscous forces are much LESS than inertial forces) AND uniform density flow, the circulation is conserved.
2)This implies (by some arduos vector calculus manipulations) that the vorticity of each fluid...
heres the problem i was working on
http://i14.photobucket.com/albums/a322/guitaristx/plane.jpg
heres my work
http://i14.photobucket.com/albums/a322/guitaristx/planework.jpg
do my FBD's look ok?...and I am trying to figure the velocity of B first,
does my a-sub-n look ok?...and to...
I've been trying to conceptualise accurately the lift forces upon an aircraft in physics terms, for a simulator flight manual I've been working on.
What I've got from some rudimentary flight training is that low pressure above the wing rather than high pressure below it causes lift, obviously...
For some time I've been thinking of making a round disk shaped model aircraft that would appear to have low drag, maximum internal carrying space, and maximum load carrying ability. As you can guess, there is little available on such a design, other than the Pancake, built at the end of WWII...
Hopefully I have posted this in the correct section;
Can anyone help with the equation(s) & assumptions required to specifically calculate the landing G load of a modern jet aircraft.
I'm trying to calculate the G deceleration rate of an aircraft on landing based on the initial vertical...
Homework Statement
You are a pilot on an aircraft carrier. You must fly to another aircraft carrier, now 1450 km at 45 degree of your position, moving at 56 km/hr due east. The wind is blowing from the south at 72 km/hr. Calculate the heading and airspeed needed to reach the carrier 2.5 hour...
Homework Statement
The pilot of an aircraft wishes to fly due west in a 50.0 km/h wind blowing toward the south. The speed of the aircraft in the absence of a wind is 205 km/h.
a.In what direction should the aircraft head?
b. What should its speed be relative to the ground?
Homework...
I am working on modeling a power system on an aircraft right now, the problem is that I have loads that are constant power drawing no matter the voltage. They will draw 5kilowatts no matter 28 volts or 22 volts. My problem is modeling them. I can model them at one particular voltage but I want a...
To go off on a tangent - I am watching a discovery channel program about the F22 fighter. A pilot (who looks about 15) is describing how the aircraft's engine is unique because it can vector thrust for manouverability and can fly supersonic without afterburner.
I suppose that's true now that...
This is a differential equations problem that I've been having some trouble with. A plane is flying and always pointing towards point (0,0) on an xy plane. Wind is constantly blowing North (positive y direction). The wind speed and speed of the aircraft through the air are constant.
(a)...
hey
Was wondering.
http://en.wikipedia.org/wiki/Aircraft_carrier
1) Does USA really have 12 4.5 billion USD Carriers ? or are some from the cold war ?
Are Cold war carriers of any use ? (like to carry helicopters) ?
2) Does france really have only 1 aircraft carrier now ? That seems small...
Homework Statement
The Attempt at a Solution
Vch = Vce + Vhe Do I have this correct?
I am guessing I need to find the velocity of the carrier with the respect to earth, and also find the velocity of the helicopter with respect to earth. Than with these two answers I can find...
Anyone know how long a typical let's say news helicopter can last in the air given how much fuel it holds?
I am not sure but I heard a news helicopter or a police helicopter probably won't last more than 3 hours in the air.
Some military transport helicopters can only do about 2 and attack...
A friend of mine who has a lot of experience with aircraft tells me the following:-
His premise seems to be that something changes when your feet are off the floor.
I think what he is saying is incorrect and that the distance jumped will be the same in either direction as the whole...
How do you figure out how fast an aircraft can travel, in Km/H ,if given the weight and the thrust.
For example: the aircraft weighs 3,100 lbs and has 20,000lbs of thrust
i thought it was 20,000/3,100= 6.5m/s/s which would be 23km/h ?
but a 747 weighs around 850,00 lbs and has...
I selected two motion problems:
1) Aircraft landing
2) Ball falling onto the gound
Using conservation of mechnical energy principles I need to fully expain and justify my reasons why its more suitable than applying Newton's laws of motion.
I have already said
a) Newton laws of...
Pleaseeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeeee
I have to present a paper on Aircraft materials and I have only one month left to prepare...
I've split my paper into 3 parts and for the third aspect,I need to know the material details of Jumbo Jets like 787...
I was reading about some recent announcements by Aeros and their competitor SkyCat, both of whom are seeking to marke large hybrid airships as a means of transporting very heavy payloads through the air.
I'd like to ask, what would be the best engineering solution to safely transport the...
I have been working on a problem trying to solve the turn diameter of an aircraft in a steady state level turn. I have been using the standard equations for turn radius and rate of turn. The formulas I am using are:
1) Turn Radius = (Velocity*Velocity)/(11.26 *Tan (bank Angle)) , velocity...