Curated OER
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.
Curated OER
Mach Number Problem Set
Students read a textbook about aerodynamics. They find out the definition of Mach number. They complete problems designed to demonstrate their ability to solve Mach number equations.
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Drag Equation - Level 1
Young scholars, after reading the Drag Equation page from the NASA Web site, demonstrate an understanding of this equation and how drag is dependent on the variables included in the equation.
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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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PROBLEMS/SOLUTIONS
Students choose an interesting problem related to space travel and then design a plan to solve the problem. They present their solution to the class.
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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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The Lift Equation Problem Set
Students, after reading the Lift Equation page from a NASA Web-based textbook, demonstrate an understanding of the lift equation by answering questions.
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Altitude and Flight Forces
Learners use the World Wide Web to access and use FoilSim. They also use the World Wide Web to access the NASA Glenn Web site for information relative to the factors involved with the flight of an airplane.
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Using 3-D Models for Code Validation with FoilSim
Students use FoilSim to complete the activity to create tables of data sets comparing the lift values for a 3-D model of a symmetrical wing section to the values predicted by the FoilSim software.