28 p51 mustang coloring page
p51 mustang coloring page
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I'm Jake O'Neal, creator of Animagraffs.
And this is How a P-51 Mustang Works., I've chosen the definitive P-51D model, which
entered service in late 1943 as a very capable , all around fighter and long-range bomber escort
that helped grant Allied forces air superiority. , Let's start with the frame and outer skin. , Hundreds of panels are riveted to a
supporting structure called the airframe. , These parts are mostly made of aluminum
for strong yet lightweight construction. , Sturdy beams and cross-braces support
the engine. Hardened steel armor plates , in front and behind the cockpit offer some
protection to the pilot from enemy gunfire. , The fuselage has longerons that extend the
length of the frame, and horizontal formers. , Ribs and spars make up the wing structure,
with smaller stringers for additional support. , Aluminum frame components get their yellow
coloring from a special protective coating. , Exterior parts might have a
range of different finishes , designed to smooth out body work and rivet
bumps for a faster and better handling airplane. , LANDING GEAR &
GROUND STEERING , The main landing gear is
controlled by a hydraulic actuator. , A separate actuator manages the clamshell doors. , A moving lock pin secures the mechanism
in place when the gear is down. , There's a shock absorber inside the
support arm and a brake in each wheel. , The pilot can steer the plane while grounded
by pressing the left or right rudder pedals, , which also engages corresponding wheel brakes.
The rear landing gear mechanism is more complex. , The assembly is retractable
just like the main landing gear. , However, the rear wheel can operate in "locked"
mode, which links its rotation to the airplane's , rudder. As the rudder rotates, the cables
tighten in turn, turning the wheel left or right. , Cables pass through a spring loaded tensioner , so they remain taught but can still
move with the rear shock absorber. , ENGINE
The P-51D is powered by a Packard V-1650 , Merlin engine. It has 12 cylinders in
a 60 degree V formation, and produces , 1,400 hp, with a top speed of 430-plus mph.
Air enters through an intake under the , nose section, and is forced through a large
centrifugal (or circular shaped) supercharger. , Engine cooling is handled with a radiator placed
just behind the wings, under the fuselage. , The low-hanging scoop is separate from
the airplane body to capture cleaner air , that's further from turbulence-causing
exterior features and propeller air. , The placement also allows a longer duct
to take advantage of the Meredith effect, , where hot air from the radiator's normal function , can be used to produce thrust – recovering as much
as 90% of the drag caused by the radiator scoop. , The radiator exhaust port has an
adjustable flap to regulate outflow. , A separate engine oil cooler with its own
exhaust flap also resides in the scoop. , An engine oil tank is mounted to the firewall. , A front-mounted tank holds
circulating radiator fluid. , Exhaust exits through short, angled nozzles. , Fuel tanks in each wing hold 92
gallons each, with an additional , 85 gallon fuselage tank behind the cockpit. , Optional drop tanks can be mounted
to the underside of each wing , at 110 gallons each, pushing the total possible
fuel capacity to a whopping 489 gallons, , with a resulting range of 1,650 miles. A
fighter aircraft with the range to reach far , into enemy territory proved to be a
major game-changer in the war effort. , PROPELLER
The propeller is connected , directly to the engine through a relatively
simple gear set. There is no transmission , or gear shift like you'd find in almost any land
vehicle. Instead, blade pitch can be controlled. , For example, at takeoff the blades
are angled perpendicular to the , airplane for a strong forward pull
in little to zero existing airflow. , While cruising at speed, that same pitch
would create a barrier, causing drag , and slowing forward movement. So the blades are
angled more in line with the direction of travel. , ARMAMENTS , There are six Browning .50 caliber machine
guns mounted in the wings, with three on each , side. They're controlled by a stick mounted
trigger which, when activated, fires all guns , simultaneously. Ammo capacity is 1,880 rounds,
with a fire rate of about 30 rounds per second. , With all six guns firing together, that's
about 30 seconds total firing time. , There's no cockpit indicator for rounds remaining. , A camera mounted in each wing can be set to turn
on when guns are fired to record the result. , A single removable bomb rack can be fitted to
the underside of each wing to cary 100, 250, , or 500 pound bombs. Alternatively, these racks
can carry droppable fuel tanks. Six rockets can , also be loaded, with three on each wing. Or ten
total rockets, when the bomb rack is not in use. , COCKPIT
These planes were designed , for technical war operations, and were not
expected to be comfortable as a first priority. , Some pilots reported having to be
lifted out of the cockpit after deep , range missions in such cramped quarters.
Controls and gauges cover every surface, , leaving space only for the pilot's
body and bulky flight gear. , Starting from the left side of the cockpit,
there's a flare gun case and a flare gun , mounting tube that extends through the plane to
the exterior. Below that, a wing flap control , lever sets the position of the main wing flaps.
A set of dials controls various on the rudder, , ailerons, and elevators.
For example, if more fuel , gets used in one wing tank than the other, the
airplane may become unbalanced and "pull" in , unwanted directions. The appropriate trim tab can
be adjusted to counter the unwanted attitude so , the pilot doesn't have to fight against the
controls to constantly balance the craft. , The radiator and oil cooler switches
control the previously shown , exhaust flap positions for those systems.
Also on this panel, a landing light switch , for lights that fold out of the main landing gear
bay, and a switch for the left side cockpit light. , The landing gear lever is down by the pilot's left
leg, as well as the left wing fuel tank gauge. , The bomb salvo lever mechanically releases bombs , as opposed to the electrically
activated button on the stick. , The fuel to air mixture, propeller RPM, and
engine throttle controls are grouped together. , The propeller RPM lever setting attempts to
maintain constant propeller rotational speed, , automatically altering things like engine
throttle or propeller blade pitch to do so. , The propeller and the air around it functions , something like an automatic transmission does in
a car. And in the same way, a car's engine RPM's , aren't always directly related to the
actual speed the car may be moving. , So for an airplane, controlling propeller
speed is the best way to control airspeed. , Moving to the pilot's forward
view, we see the flight stick, , with a bomb release button on top,
and the gun trigger at the front. , Generally speaking, flight stick left
or right movement will roll the plane. , Stick forward or back movement alters the pitch.
The left and right rudder pedals manage yaw. , Beyond the stick we see the main fuel
shut-off lever, and a fuel tank selector dial. , The fairing door emergency pull lever releases
landing gear in case of a motorized malfunction. , Once released, gear can be manually
locked by yawing the plane left or right. , A hydraulic pressure gauge is situated nearby. , A warning light above the emergency lever
indicates if landing gear doors are open. , Separate warning lights indicate left
and right landing gear lock status. , The various switches and knobs
nearby control armaments settings. , Bombs can be released all together or in a
train. Guns can be set as single fire, burst, , or fully automatic. The amount of rounds per
burst can also be set with the corresponding dial. , On the left of this panel, there's the engine
ignition switch. In the center, the parking brake. , The left switch bank has supercharger boost
control and other engine specific settings. , On the right, the oxygen blinker moves with the
pilot's breathing to very accurately indicate , oxygen consumption with each breath. Pilots need
specific oxygen indicators due to the dangers , of consuming too much or too little oxygen,
which can cause confusion and pilot error. , A pressure gauge to the right
indicates oxygen system pressure. , The oxygen regulator controls flow to the pilot. , There are left and right
positionable lights for illumination. , The yellow line across the
dashboard separates flight , control related gauges into their own section.
From the left, we have the altimeter for altitude, , the airspeed indicator, the directional gyro
and compass which are used together to maintain , a specific course of travel. The bank and turn
indicator shows the plane's current attitude. , The artificial horizon indicates
ground angle relative to the plane. , Outside the white line there's the clock, a
suction gauge to monitor vacuum pressure since , many of these gauges and instruments use
vacuum pressure differences to function. , The manifold pressure gauge tracks internal
engine pressure. The propeller might be turning , at the same speed but requiring lots of engine
force, so manifold pressure must be monitored. , There's a coolant temperature gauge, a
tachometer for engine RPMs, a carburetor air , temperature indicator to make sure the engine
air intake stays within a reasonable range, , and an oil and fuel pressure gauge. , Turning to the pilot's right side we see
electrical and radio equipment controls. , Including an ammeter to monitor electrical
current from the plane's generator. There , are switches for generator and battery disconnect,
left and right gun heaters, and position lights. , Red, green, and amber position lights
on the underside of the right wingtip , can display codes to indicate
friendly aircraft approach at night. , Late model P-51D's had a tail radar system
to warn of aircraft behind the plane. , A radio frequency tuner and
headphone hook-in sits beneath that. , The last couple modules are radio control units, , and an IFF system used to signal a friendly
aircraft to external radar systems. , The right wing fuel tank gauge
is on the floor by the seat pan. , The canopy crank is also on this
side, with an emergency release lever. , Just behind the pilot's left ear there's the
fuselage fuel tank guage, various electronic , devices inducing radio and radar modules,
and behind that, the oxygen tank storage bay. , Coming back to the pilot's
view, we see the gunsight. , A standard straight-ahead sight, marked with
the "plus" sign, and a compensating sight are , projected from horizontal lenses
onto a thin pane of angled glass. , The pilot sets the wingspan dial at the front
to correspond to the target's wingspan, measured , in feet. A twist grip on the throttle brings
the compensating sight's diamond ring into an , imaginary circle around the target's wings. This,
combined with the center dot over the target's , cockpit, automatically calculates bullet range and
arc as both planes move through the air at speed. , PILOT
During the era of the P-51, , regulations for pilot's gear were a bit more
open to individual preference, so I've put , together a generalized equipment set. The pilot
wears a leather helmet with earphones built in. , Also a set of goggles, and an oxygen mask with a
built-in microphone just above the breathing tube. , The pilot wears a vest
style yellow life preserver. , Parachute rigging straps encircle the
pilot's torso and legs, and extend to a , parachute back pad that was often packed with
first aid items and a one-person life raft. , The pilot's parachute is packaged beneath the
seat cushion. All of these things are attached , to the parachute rigging and follow
the pilot in the event of a bailout. , The jacket and coveralls are either wool or
cotton, paired with warm leather gloves and boots.
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