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Flight Adventure Deck Interactive Devices

Coin and Feather

Learning Objective: To understand the principle behind Galileo’s Law of Falling Bodies (Gravity).

Method: The device consists of two clear, hollow acrylic tubes mounted on a vertical turntable. Each tube contains a coin and light paper discs or feathers. One tube contains ambient air; the other is a vacuum (the tube has no air.) When rotated 180°, the coin hits bottom before the feather in the air-filled tube; in the evacuated tube, the coin and feather hit bottom simultaneously.

Falling Bodies Device

Learning Objective: To understand the principle behind Galileo’s Law of Falling Bodies (Gravity).

Method: The device consists of a pair of vertical acrylic tubes with a plunger-operated release mechanism at the top which serves to release a pair of tennis balls simultaneously into the tubes. One ball has been filled with BBs, making it noticeably heavier than the other. When placed into their recesses at the top of the tubes and released, both balls reach the bottom of the tubes simultaneously.

Galileo’s Pendulums

Learning Objective: To understand the principle behind Galileo’s Law of Falling Bodies (Gravity).

Method: The device consists of a pair of pendulums: one having a bob of cork; the other a bob of lead.When pulled back and released simultaneously, the operator will observe that the initial period (or swing) of both bobs is equal, despite their obvious difference in mass.

Space Scale

Learning Objective: To understand the relationship between weight and mass. (Gravity)

Method: The device consists of a scale and console with touchpads for ten locations in the solar system: Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, Pluto, and Earth’s moon. When standing on the scale, the operator can select any of these locations and observe how his or her weight changes according to the gravitational pull created by the different masses of the planets.

Frictionless Air Track

Learning Objective: To understand the principles contained in Newton’s Laws of Motion: Inertia, Acceleration and Action-Reaction.

Method: The device consists of a 1.5 meter long extruded aluminum beam connected to an air source. Air is blown through small holes at regular intervals the length and width of the beam, creating an air cushion along its surface. Two aluminum "cars" float freely on the air cushion when activated, allowing the operator to accelerate them in a variety of ways in a virtually frictionless environment. One car is equipped with a balloon-nozzle attachment which allows it to be self-propelled. Removable weights can be fitted to the cars to alter their masses for class group experiments.

Measuring Air Pressure Device

Learning Objective: To understand the relationship between air pressure and altitude in Earth’s atmosphere.

Method: The device consists of a large acrylic cylinder mounted on a cabinet with a rubber diaphragm in its base. A hand-operated wheel connected to a cam pushes up or pulls down on the diaphragm, increasing or decreasing pressure within the cylinder. A calibrated manometer tube provides a visual display of the atmospheric pressures at key geographic elevations on Earth.

Pressure Versus Altitude Device

Learning Objective: To understand the relationship between air pressure and altitude in Earth’s atmosphere.

Method: The device consists of a series of weighted bars, each representing the weight of a 1" square column of atmosphere at a given altitude. Operators can compare the atmospheric weights or pressures between sea level and intervals up to 50,000 feet above sea level (MSL).

Magdeburg Hemispheres

Learning Objective: To understand that air is matter which has mass and occupies volume (atmospheric pressure.)

Method: The device mimics an experiment conducted by Otto von Guericke in Magdeburg, Germany in the 17th century. Two machined aluminum hemispheres are mounted to the top of a cabinet, one fixed and the other mounted on a vertical sliding track which allows it to be slid up and down to form a complete sphere. With the stopcock on the upper hemisphere closed and the two hemispheres placed together, a button-actuated vacuum pump removes the air from within the sphere and prevents pulling the two hemispheres apart.

Descartes Divers

Learning Objectives: To understand Archimedes’ principle of displacement (buoyancy) and gas volume vs. pressure (Boyles Law).

Method: The device consists of a water-filled cylinder topped by a lever-operated diaphragm. Two glass Cartesian "divers" or air-filled buoys are suspended in the cylinder. Operation of the lever either increases or decreases pressure on the water column, directly compressing or expanding the volume of air within each diver and causing it to ascend or descend.

Helium Balloons

Learning Objective: To understand the principle of displacement (buoyancy).

Method: The device consists of a tethered, helium-filled weather balloon beneath which is suspended a small basket. The operator can experiment with different payloads to achieve positive, neutral or negative buoyancy.

Weight of Gases Device

Learning Objective: To understand the variations in density and weight of the volume of given gases that are components of atmospheric air.

Method: The device consists of a series of weighted bars each representing the weight of 100 cubic feet of a given gas: Oxygen, Carbon Dioxide, Nitrogen, Argon, Hydrogen and Helium.

Bernoulli Blower

Learning Objective: To observe an application of Bernoulli’s Principle.

Method: The device consists of a cabinet-enclosed blower and a swiveling air exhaust plenum and rubber ball. When actuated, exhaust air holds the ball in suspension 2-3 feet above the plenum. Operator can rotate plenum to 45° from the vertical and observe that ball remains suspended within the air column.

Bernoulli Demonstrator

Learning Objective: To understand Bernoulli’s Principle of fluid dynamics and its application to aerodynamics.

Method: The device is a wind tunnel equipped with a clear test section and a bank of fluid-filled manometer tubes. The test section contains yellow-colored shapes which form a venturi nozzle and a fixed airfoil. The operator can select one of three airspeeds and observe how the air pressure changes at different points within the venturi and along the airfoil’s surface.

Drag Demonstrator

Learning Objective: To understand the relationship between an object’s shape and the amount of resistance to air flow (drag) it causes.

Method: The device is a wind tunnel equipped with three different shapes: cylinder, sphere and teardrop which can individually or collectively be exposed to the air stream through the wind tunnel. Each shape is instrumented to generate a digital proportional signal for the amount of drag induced in it by the force of the air against it.

Angle of Attack (AOA) Wind Tunnel

Learning Objective: To understand the relationship between angle of attack, lift, drag and stall.

Method: The device consists of a wind tunnel equipped with a clear test section containing a yellow-colored airfoil. The airfoil is mounted on a transverse bearing which allows it to be adjusted in pitch relative to the air flow. Operator can vary airspeed and angle of attack to observe resulting lift, drag and onset of stall. LED readouts indicate airspeed, lift and drag; red film streamers attached to the airfoil flutter to indicate stall.

High-Lift Device Wind Tunnel

Learning Objective: To understand how high-lift devices affect lift, drag and stall speeds.

Method: The device consists of a wind tunnel equipped with clear test section containing a yellow-colored airfoil with trailing edge flap and leading edge slat. The operator can adjust airspeed and angle of attack, and extend or retract the flap to observe resulting lift, drag and onset of stall. LED readouts are provided for airspeed, lift and drag;. red film streamers attached to the airfoil flutter to indicate stall.

Aircraft Control Stick

Learning Objective: To illustrate how the movement of an aircraft control stick affects the movement of an aircraft aileron.

Method: The device consists of a standard aircraft control stick rigged to operate the left wing aileron of a wing structure mounted overhead.

Captive Mentor Wind Tunnel

Learning Objective: To illustrate how the movement of aircraft control surfaces (elevator, aileron and rudder) affects the control and stability of an aircraft in the axes of pitch, roll and yaw.

Method: The device consists of a large wind tunnel containing a 1/16 scale T-34C "Turbomentor" remote-controlled model. Operator sits at a control console equipped with stick, throttle and rudder pedals and flies model in the wind tunnel. Limited control authority and area restrict movement to approximately 3 feet up and down and 3 feet left and right.

Interactive Flight Simulator

Learning Objectives: To understand how control movements affect aircraft performance: airspeed, altitude, heading, rate of descent and rate of climb. To understand the basic variables essential to piloting an aircraft: attitude, airspeed and power. To appreciate the level of situational awareness and eye-to-hand coordination required to pilot an aircraft.

Method: The flight simulator is a highly interactive, highly realistic depiction of the flight environment. The hardware is configured to resemble a hybrid F-18/F-16 jet aircraft cockpit with a full set of controls and basic instruments. Out-the-window view from the cockpit is a wide-angle projection 10 feet wide by 8 feet high. Software may be configured to provide a concise, "canned" flight program which takes operator through a specific, limited profile (e.g. final approach to carrier landing), or it can be configured to provide an open flight program of unlimited duration and mission profiles.

Wright Cyclone R-1820 Radial Engine

Learning Objective: To illustrate the mechanical operation of the piston, crankshaft and supercharger of the Cyclone engine.

Method: An operating cutaway of the Cyclone engine shows the mechanical movements of one of the nine pistons and its connecting rod to the engine crankshaft and reduction gearing to the propeller driveshaft. The centrifugal impeller for the supercharger is also displayed.

Westinghouse J-34 Turbojet Engine

Learning Objective: To illustrate the mechanical operation of the compressor and power turbine sections of a turbojet engine.

Method: An operating cutaway of the J-34 engine shows the mechanical rotation of the driveshaft and the compressor and power turbine sections it connects.

Fiberoptic Display of the J-34

Learning Objective: To understand how a gas turbine engine operates: the four stages of power production and how the engine converts fuel and air into thrust.

Method: The fiberoptically lit graphic of the J-34 cutaway is keyed to buttons on a visitor-operated console which correspond to different sections of the engine and steps in the power-production cycle.

Prop Versus Rocket Display

Learning Objective: To understand the advantages and limitations of propeller versus rocket propulsion as a function of altitude.

Method: The device consists of a pair of spindle-mounted rotating metal arms enclosed inside a large plexiglas dome. Mounted on the end of the top arm is a 1:200 scale model of the Space Shuttle; the other arm mounts a 1:48 scale model of a Navy F4F airplane. Low pressure air is routed from a compressor in the device base to air jets in both ends of the Shuttle’s arm; a 3 volt DC power source energizes an electrical motor in the F4F, driving its propeller. The operator energizes both aircraft and observes them "flying" in circles. Actuating a vacuum pump/motor evacuates air from the dome, simulating a climb in altitude until a virtually air-less environment is reached. A timer-actuated cutoff stops the pump and allows air back into the chamber.

Propeller Display

Learning Objective: To observe how a propeller is designed like a "wing with a twist."

Method: The device consists of a series of cross-sections of a Hartzell propeller blade from a T-34 aircraft. Visitors can handle and examine the sections and compare their shapes with others taken from the same blade.


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National Museum Of Naval Aviation

1750 Radford Blvd. Pensacola, FL 32508
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