posted on Oct, 8 2003 @ 05:10 AM
F-16 Fighting Falcon:
The F-16 Fighting Falcon is a compact, multirole fighter aircraft. It is highly maneuverable and has proven itself in air-to-air combat and
air-to-surface attack. It provides a relatively low-cost, high-performance weapon system for the United States and allied nations.
In an air combat role, the F-16's maneuverability and combat radius (distance it can fly to enter air combat, stay, fight and return) exceed that of
all potential threat fighter aircraft. It can locate targets in all weather conditions and detect low flying aircraft in radar ground clutter. In an
air-to-surface role, the F-16 can fly more than 500 miles (860 kilometers), deliver its weapons with superior accuracy, defend itself against enemy
aircraft, and return to its starting point. An all-weather capability allows it to accurately deliver ordnance during non-visual bombing
conditions.
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History:
The air war experience in Vietnam, where the lack of maneuverability of US fighters at transonic speeds provided advantages to nimble enemy
fighters, was the stimulus for the Lightweight Fighter program. The Air Force and designers of the Lightweight Fighter therefore placed great emphasis
on achieving unprecedented transonic maneuver capability with excellent handling qualities.
In January 1972, the Lightweight Fighter Program solicited design specifications from several American manufacturers. Participants were told to tailor
their specifications toward the goal of developing a true air superiority lightweight fighter. General Dynamics and Northrop were asked to build
prototypes, which could be evaluated with no promise of a follow-on production contract. These were to be strictly technology demonstrators. The two
contractors were given creative freedom to build their own vision of a lightweight air superiority fighter, with only a limited number of specified
performance goals. Northrop produced the twin-engine YF-17, using breakthrough aerodynamic technologies and two high-thrust engines. General Dynamics
countered with the compact YF-16, built around a single F100 engine.
The evolution of the YF-16 design at LMTAS included studies of configuration variables such as wing design, maneuvering devices, number and location
of engines, control surfaces, number and location of tail surfaces, and structural concepts. As the configuration options matured, two candidate
configurations competed for priority. The first configuration was a simple wing, body, and empennage design, while the second design was a
twin-tailed, blended-wing body with vertical and horizontal tails on booms. The LMTAS team selected the best features of both configurations for the
final YF-16 design. After considerations of performance, stability, and control were addressed, the YF-16 configuration incorporated a rather wide,
blended forebody that produced strong vortices at moderate angles of attack. LMTAS had attempted to weaken the strength of the vortices by promoting
attached flow, but these attempts were not successful.
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Design:
In designing the F-16, advanced aerospace science and proven reliable systems from other aircraft such as the F-15 and F-111 were selected. These
were combined to simplify the airplane and reduce its size, purchase price, maintenance costs and weight. The light weight of the fuselage is achieved
without reducing its strength. With a full load of internal fuel, the F-16 can withstand up to nine G's -- nine times the force of gravity -- which
exceeds the capability of other current fighter aircraft.
The aerodynamic configuration of the F-16 is a highly integrated synthesis of such components as wing, fuselage, and inlet, with the aim of achieving
maximum favorable flow interaction with subsequent optimization of overall performance. Configuration features include a cropped delta wing mounted
near the top of the fuselage with large strakes extending forward from the leading edge to the sides of the fuselage. A single vertical tail is
utilized together with a small fixed ventral fin located on the bottom of the fuselage. The all-moving horizontal tail is mounted in the low position
and incorporates a small amount of negative dihedral.
A fixed-geometry, chin-mounted inlet supplies air to the single Pratt & Whitney F100-PW-200 turbofan engine, which is a variant of the same power
plant utilized in the F-15. Since the forward portion of the fuselage provides some external flow compression, reasonable inlet efficiency is obtained
even at a Mach number of 2.0. Good inlet efficiency through a wide range of angle of attack is ensured by the location of the inlet on the bottom side
of the fuselage at a fore-and-aft location behind the forward intersection of the wing strakes with the side of the fuselage.
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Israeli F-16D showing the enlarged spine on some Israeli F-16D:s that houses SEAD and defence electronics.
Good pic showing F-16s M61 A1 Vulcan 20mm Gatling cannon installation.
Hear Vulcan firing!!!
USAF F-16C armed with two AIM-120 AMRAAM BVR missiles.
As one can see the F-16s have had their share of the wars.. with some good success in air-to-air combat.
(this Israeli machine has 5 Syrian kills.)
Or like this Israeli F-16 which has 6,5 kills (one shared..) and was one of the aircrafts that bombed
the Osirak nuclear reactor in Iraq.
(each attacking aircraft carrying 2 2000lb MK84 bombs.)
Major feats for aircraft that was 'only' designed to replace F-5s and counter MiG-21s..
Latest F-16 C/D Block 60+ (and F-16 I) aircrafts really are more like strategic strike aircrafts than tactical light fighters..
Good exambles just how good of a an aircraft F-16s are:
F-16s were build to counter MiG-21s, yet they have least twice shot down MiG-25s Least 1 Iraq MiG-25 by USAF F-16 using AMRAAM BVR missile in 1992 and
at least 1 Syrian MiG-25 by Israeli F-16..
Build to counter mach 2 MiG-21 light fighter, capable on taking mach 3 heavy MiG-25 Foxbat..
www.f-16.net...