The Letov Š-14 was a single-seat, single-engine aircraft, designed and built in
Czechoslovakia
Czechoslovakia ( ; Czech language, Czech and , ''Česko-Slovensko'') was a landlocked country in Central Europe, created in 1918, when it declared its independence from Austria-Hungary. In 1938, after the Munich Agreement, the Sudetenland beca ...
in the early 1920s. Originally intended as a
biplane
A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While ...
fighter, it was later modified into a monoplane and entered as a contestant in a speed competition.
Design and development
The Letov Š-14 was designed alongside the
Letov Š-13, sharing its Škoda licence-built 300 hp (224 kW) Hispano-Suiza 8Fb water-cooled V-8 engine but not its thick
airfoil
An airfoil (American English) or aerofoil (British English) is a streamlined body that is capable of generating significantly more Lift (force), lift than Drag (physics), drag. Wings, sails and propeller blades are examples of airfoils. Foil (fl ...
wings. Like the Š-13, it was intended as a single-seat
biplane
A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While ...
fighter aircraft
Fighter aircraft (early on also ''pursuit aircraft'') are military aircraft designed primarily for air-to-air combat. In military conflict, the role of fighter aircraft is to establish air supremacy, air superiority of the battlespace. Domina ...
. It was of mixed construction, with wooden wings and a metal-framed
fuselage
The fuselage (; from the French language, French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds Aircrew, crew, passengers, or cargo. In single-engine aircraft, it will usually contain an Aircraft engine, engine as wel ...
.
The wings, mounted without
stagger, were straight edged with a constant
chord and blunt
wingtips. It was a
single bay biplane with a pair of
interplane strut
In aeronautics, bracing comprises additional structural members which stiffen the functional airframe to give it rigidity and strength under load. Bracing may be applied both internally and externally, and may take the form of struts, which act in ...
s on each side. These were straight and near parallel, but converged a little towards the narrower chord lower wing. The upper wing was braced to the fuselage with a
cabane immediately ahead of the open
cockpit
A cockpit or flight deck is the area, on the front part of an aircraft, spacecraft, or submersible, from which a pilot controls the vehicle.
The cockpit of an aircraft contains flight instruments on an instrument panel, and the controls th ...
, situated below the wing
trailing edge
The trailing edge of an aerodynamic surface such as a wing is its rear edge, where the airflow separated by the leading edge meets.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 521. Aviation Supplies & Academics, 1997. ...
.
[
The Hispano drove a two-blade ]propeller
A propeller (often called a screw if on a ship or an airscrew if on an aircraft) is a device with a rotating hub and radiating blades that are set at a pitch to form a helical spiral which, when rotated, exerts linear thrust upon a working flu ...
with a pointed spinner Spinner may refer to:
Technology
* Spinner (aeronautics), the aerodynamic cone at the hub of an aircraft propeller
* Spinner (cell culture), laboratory equipment for cultivating plant or mammalian cells
* Spinner (computing), a graphical widget in ...
; it was cooled by a rectangular radiator
A radiator is a heat exchanger used to transfer thermal energy from one medium to another for the purpose of cooling and heating. The majority of radiators are constructed to function in cars, buildings, and electronics.
A radiator is always a ...
on each side of the fuselage between the wings. The fuselage was flat sided with rounded decking, tapering aft to the mid-mounted tailplane
A tailplane, also known as a horizontal stabilizer, is a small lift (force), lifting surface located on the tail (empennage) behind the main lifting surfaces of a fixed-wing aircraft as well as other non-fixed-wing aircraft such as helicopters ...
, where the vertical tail was broad and low. The Š-14 landed on a fixed conventional tailskid undercarriage.[
The Š-14 first flew in 1924 but Letov quickly decided to concentrate their fighter development efforts on the Letov Š-20 which flew the following year.][ Instead, the Š-14 was rebuilt as a ]cantilever
A cantilever is a rigid structural element that extends horizontally and is unsupported at one end. Typically it extends from a flat vertical surface such as a wall, to which it must be firmly attached. Like other structural elements, a cantilev ...
monoplane
A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple wings.
A monoplane has inherently the highest efficiency and lowest drag of any wing con ...
to take part in the Third Speed Contest of 1924. At that event it recorded a speed of .[
]
Specifications (biplane)
References
{{DEFAULTSORT:Letov S-14
1920s Czechoslovak fighter aircraft
Letov aircraft
Single-engined tractor aircraft
Parasol-wing aircraft
Aircraft first flown in 1924