Thin airfoil delta wing.
Answer:
There is no "best" configuration. It depends on what the aircraft is required to do.
Take a look at, for example, the wing on an F-104 Starfighter compared to that of Concorde. Each of these have a wing designed to be "best" for the operations that the aircraft is required to perform.
The best location for spoilers on an aircraft is the top of the wing. this is because spoilers help slow aircraft down so the top would be the best place.
I. Frank Sakata has written: 'Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft' -- subject(s): Aerodynamics, Transonic, Supersonic planes, Transonic Aerodynamics
Swept wings are preferred in supersonic aircraft to facilitate vertical take off and reduce runway length during take off.
A straight wing is good for a low-powered, slow moving aircraft. A straight, thick wing is good for short takeoff and landing aircraft, and high-speed, high-thrust aircraft need a swept wing.
Christopher A. Lee has written: 'Design and testing of an oblique all-wing supersonic transport' -- subject(s): Transport aircraft, Wind tunnel tests, Propulsion system configurations, Oblique wings, Supersonic wind tunnels, Wind tunnel models, Aircraft design, Supersonic transports 'I, digital' -- subject(s): Family archives, Personal archives, Digitization, Digital preservation, Archival materials
A monoplane is an aircraft design characterized by having a single main wing structure, as opposed to biplanes, which have two wings stacked one above the other. This configuration allows for improved aerodynamic efficiency and performance, making monoplane designs more common in modern aviation. Monoplanes can vary in wing shape and size, but the key feature is the singular wing structure that supports the aircraft's flight.
They test it in the wind tunnel. If the design fails to pass the test they make an another design. By testing and testing they come up with the design at last.AnswerEngineers begin a wing design by identifying the purpose of the airplane and the speeds and weights that it will operate. An airplane that will fly slow may have a thick wing or a long & tapered wing. A fighter aircraft that will fly supersonic will have a thin wing and short and stubby. Then they adjust the shape of the wing to obtain the Lift and Drag and airflow that is needed for the design.
A fixed-wing aircraft is an aircraft which has wings that are attached to the aircraft and do not move. The term is used to differentiate airplanes from other types of flying vehicles such as lifting-body aircraft (balloons and blimps) or rotary aircraft such as helicopters and auto gyros. All airplanes are considered fixed-wing aircraft and even swing-wing or otherwise moving-wing airplanes are usually referred to as being in the fixed-wing category of aircraft.
AUTOROTATION is only for Rotary Wing aircraft...not fixed wing
Most civil aircraft have their jets either under-wing or in the tail or on the side of the tail. Most cargo aircraft and bombers have the same configuration. The B-2 has engines buried in the wing. Most fighters used to either have the jet embedded in the body or on the side.
Approximately 37 US fixed-wing aircraft and 23 rotor-wing aircraft were lost during DS. Approximately 15 of those fixed-wing aircraft & 18 of the rotor-wing aircraft were lost to operational causes (accidents).
Heavy, clean, and slow VORTEX STRENGTH The strength of the vortex is governed by the weight, speed, and shape of the wing of the generating aircraft. The vortex characteristics of any given aircraft can also be changed by the extension of flaps or other wing configuration devices as well as by a change in speed. The greatest vortex strength occurs when the generating aircraft is heavy, clean, and slow.