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Forces on an Airplane and Resulting Motion
Students read from a NASA Web-based textbook, then students demonstrate an understanding of the text by answering questions about the forces on an airplane and their resulting motions.
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Cruising Aircraft and Balanced Forces
Students, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to questions involving cruising aircraft and balanced forces.
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Beginner's Guide to Aerodynamics
Young scholars, after reading an explanation from a NASA Web-based textbook, you demonstrate an understanding of the text by applying it to questions involving the theories of how a wing produces lift.
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Trimmed Aircraft
Students, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to the calculations involving the motion of an airplane.
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Aircraft Motion
Young scholars, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to the calculations involving the motion of an airplane.
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Aircraft Motion
Young scholars, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to the calculations involving the motion of an airplane.
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Airplane Parts/Functions Problem Sets
Students label and describe the functions of the parts of an airplane. They access a NASA Web-based textbook and read a series of lessons before labeling the parts of an airplane.
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Dimensional Analysis Problem Set
Students, after studying various pages of a NASA Web-based textbook, use dimensional analysis to verify actual aeronautic equations.
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Drag Problem Set
Students read an explanation from a NASA Web-based textbook and then demonstrate an understanding of the text by applying it to calculating drag of both full-sized and model gliders.
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Calculating Range for a Constant Velocity
Learners read an explanation from the NASA Web-based "textbook", The Beginner's Guide to Aerodynamics, then use the information in combination with data from other Web sites to solve single variable equations for distance (range), time,...
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Wing Area Effects Problem Set
Students read an explanation from a NASA Web-based textbook on lift and an explanation on the FoilSim software package given below. They use FoilSim to evaluate the relationship between wing area and lift.
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Velocity Effects Problem Set
Learners, after reading an explanation on lift from a NASA Web-based textbook and an explanation on the FoilSim software package given below, use FoilSim to evaluate the relationship between velocity and lift.
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Lift/Velocity Relationship Problem Set
Students, after reading an explanation from a NASA Web-based textbook, demonstrate their ability to use, graph (using a graphing calculator), and interpret a text equation.
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Vectors in Relative Velocities Problem Set
Pupils, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of vector addition and the text by applying them to the determination of vector components and relative velocities.
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Size Effects Problem Set
Pupils, after reading the Size Effects page from a NASA Web-based textbook, demonstrate an understanding of Size Effects by answering questions.
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Density and Lift
Students, after reading from a NASA Web-based textbook, demonstrate an understanding of the text by solving problems on density and predicting which density give the most lift.
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Showing the Lift Equation
Learners read an explanation from a NASA Web-based textbook, then demonstrate an understanding of the text by using it, along with FoilSim, to complete an activity that manipulates the lift coefficient equation.
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Airspeed Problem Set
Students demonstrate an understanding of aircraft launch airspeed requirements. They read a selection on relative velocities from a NASA Web-based textbook, then calculate airspeed launch requirement problems.
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Aircraft Trajectory Problem Set
Students, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to the calculation of speed, distance, acceleration, and time in simple aircraft motion.
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Wind Tunnel Aerodynamics Problem Set
Students, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by applying it to the calculation of area, velocity, and pressure in a wind tunnel.
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Drag Equation - Level 2
Students, after reading the Drag Equation page from the NASA Web-based textbook, demonstrate an understanding of this equation and how drag is dependent on the variables included in the equation.
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Pitot Tube Problem Set
Students read a NASA Web-based text and use its information to complete an activity which uses a pitot tube to calculate the speed of an airplane.
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Center of Gravity Problem Set
Learners read a NASA Web-based text, then demonstrate an understanding of the text by using it to complete an activity on the center of gravity of a commercial cargo airplane.
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Lift Equation Problem Set
Students, after reading an explanation from a NASA Web-based textbook, demonstrate an understanding of the text by using it, along with FoilSim, to complete an activity to graph and interpret the lift equation.