the ratio of wing span to the chord of the aerofoil is ASPECT RATIO
6:1
A series of notes sounded simulanteously- for example a C- Chord which is, on a Piano- fingered 1-3-5 starting at Middle C. Chord in Math might have to deal with a section of a bridge or an airplane wing- it has a different application than the musical sense. As music is mathematical- I have given the tonal variety first.
Undisturbed flow is the flow of air approaching the wing. The angle between chord line and undisturbed flow is the geometric angle of incidence. Local flow (the relative flow you mention) is the flow actually "hitting" the wing. As the air apporaches the wing, it goes slightly downwards due to the downwash effect. The angle between chord line and the local flow is the effective angle of incidence. The above are mainly British terms so they might be slightly different in the US. Hope it helped! Break, Break; Indeed this definition is British. The angle of incidence in the rest of the world is the angle formed between the aircraft's longitudinal axis (a line along the fuselage centerline, from the nose of the aircraft to the tail) and the wing's chord (a line between the wing airfoil's leading edge and trailing edge). The angle defined in the first paragraph is the "angle of attack" (abbreviated AOA) in the rest of the world; that is, the angle formed between the free stream air and the wing chord line. All of these definitions are quite simple and make several assumptions since wing geometry is dependant on the reference system it is measured in. When a wing is being built, it is relaxed and supported in tooling jigs. The leading edge is defined in the jig system. But the aerodynamasist evaluates the wing's performance in the 1g steady state flight mode. In this system, the wing is usually bent up at the tips and the airfoils are twisted some. This creates a different LE point whilst flying. The net result is that the person needing to know must always specify for what system or condition the LE or TE point is needed.
It changes the profile of the wing and so changes the lift. If the same change is applied to both wings the plane will gain or lose height. If opposite changes are applied, one wing will drop, the other will rise and the plane will turn.
Chord refers to the distance from the leading edge of a wing to the trailing edge of a wing. Because wings are not perfectly rectangular, average chord is used and is calculated by dividing wing area by wingspan.
The chord in an aircraft is the cross-section of the wing.
the ratio of wing span to the chord of the aerofoil is ASPECT RATIO
That is hard to answer as the Fokker Dr1 Triplane had 3 wings of different Length and Chord(which is the lenght of a section of the airfoil). Also the Upper wing had a large aileron that extended the chord and the length for a section of that wing. I found a chord dimension of 3 Feet 3 & 3/8 Inches. I think that is the middle wing. Length of each Wing. Upper Wing (with aileron) =23 Ft 7 In Middle Wing = 20 Ft 6 In Lower Wing = 18 Ft 9 In Tail- Horizontal, Width = 9 Ft 10 In Tail - Length(front to back) = 5 Ft 3 In
Rudder on the wing of the plane controls the direction.
angle of attack. It is the angle between the chord line of the wing and the oncoming airflow. A higher angle of attack generates more lift but also increases drag.
It is just called the wing.
Mono plane.
To lift the plane and enable it to fly.
It provides lift to keep the plane airborne.
The angle between the chord of the wing and the longitudinal axis of the airplance is too great.
The angle between the chord of the wing and the longitudinal axis of the airplance is too great.