originally posted by: theboarman
hello everyone,first i want to say i am no aircraft engineer but i design aircraft when i am bored, which is alot in this world,anyway most get
deleted but lately i have been doing round aircraft that resemble modern ufos but with modern tech,manned and unmanned, lately i have had this idea
of a round or semi square flat wing that creates lift no matter what angle you are at, i know a circular wing that goes upward exists and has been
somewhat tested, instead of upward they would just go flat,landing and takeoff can be done with something similar to the British harrier jump jet,
useing the (what are in my designs 3-4 small ) jet engine for landing ability but also use it for some forward propulsion, some of my designs use
electric fans similar to the f35 but going out through nozzles like the harrier.
thoughts? opinions?
I'm a professional aerospace engineer and a private pilot. I design things that fly (aircraft and spacecraft) for a living. Here are a few facts
about circular wings.
What you are actually describing is an all-wing aircraft where the wing happens to have a circular planform.
A wing can generate aerodynamic lift when it's moving forward through the air with a given speed. The magnitude of the speed and the direction it's
moving taken together define the velocity vector (speed x direction). When the front edge of the wing tilts up relative to the velocity vector,
that's considered to be the pitch direction. That pitch-up creates what's called an aerodynamic angle of attack of the wing relative to the velocity
vector. That angle of attack causes the airflow over the top of the wing to be faster than the flow under the bottom of the wing and that difference
is what causes more pressure on the bottom than the top, thereby generating lift. So, no angle of attack, no lift.
When you refer to a flat disk, maybe you mean literally a thin disk that's flat on the top and flat on the bottom (a "flat plate" disk) like it was
stamped out of a piece of sheet metal. Such a disk will generate lift if it has a positive pitch angle, but it won't be very efficient. It will
generate a lot of drag compared to the lift it generates. This is why wings that are designed to fly at low subsonic speeds have a rounded nose on the
front and a sharp trailing edge. That is the classic airfoil cross-section.
There's no reason you can't have a classic airfoil cross-section on a circular planform wing to improve its efficiency, but then the wing will have a
nose and tail. It will only be efficient when it's flying nose forward and tail aft. It won't fly at all if the relative wind is cross ways or
backward over the wing. That is no different than with a conventional rectangular wing. So if you want to have a wing that's efficient as possible,
it has to have an airfoil cross-section instead of being flat, in which case, it will only fly well when the nose of the airfoil is pointed into the
wind.
The other factor that affects the efficiency of a wing is the aspect ratio, which is approximately the wingspan divided by the width of the airfoil
section. For a general aviation aircraft, the wingspan will often be approximately 10 times the width of the airfoil section (an aspect ratio of ≈
10). For a circular wing, the wingspan and airfoil width are the same, so the aspect ratio ≈ 1, and that's also lousy for efficiency.
The upshot of all this is that you can design a subsonic aircraft consisting of a flat plate circular wing, but it will have really lousy efficiency.
As the old saying goes, you can make a barn door fly if you put a big enough motor on it.
The other thing that we haven't even talked about is stability and control. Basically, a flat plate circular wing doesn't have any preferred direction
of flight in yaw, which means it is very difficult to make it fly straight and level. You either have to put massive tail surfaces on it to give it
some static stability and/or have an active stabilization autopilot (like the F-117 "wobbly goblin").
And finally, there is the weight distribution problem. In order for a flying wing to have static stability in pitch, the center of mass of the
vehicle has to be located approximately 1/4 of the way aft of the nose. For a circular wing, that means that half of the mass has to be crammed in
the forward 1/4 of the circle. That's really, really difficult to do, when you consider that the most massive parts of the aircraft are usually the
motors and the fuel.
In short, it's really, really difficult to design a circular, all-wing aircraft and even if you do, you'll have a total dog of an aircraft.
BTW, this is how we know that real flying saucer UFOs are not flying by generating aerodynamic lift. But that's a topic for another day.