Another interesting topic you can tackle is the dependence of conductivity on particle size. As particle size approaches the nano level, instead of the continuous band structure of macro-scale solids, we get slightly discontinuous structures where the continuous approximation fails and some resemblance to the atomic large energy level gaps is present. This leads to really interesting optical properties, and presumably affects the conductivity too. It's a very new topic so if you tackle it well you may not need an experiment.
Jet Performance In this first part we will utilize the drag table that you prepared in module 4. Notice that the total drag column, if plotted against the associated speeds, will give you a drag curve in quite similar way to the example curves e.
Notice also that this total drag curve directly depicts the thrust required when it comes to performance considerations; i.
For all practical purposes, we could use any propulsion system we wanted and still would come up with the same fundamental drag curve, because it is only based on the design and shape of the aircraft wings.
What thrust [lbs] would this engine have to develop in order to reach kts in level flight at sea level standard conditions?
Notice again that in equilibrium flight i. In essence, this example is a reverse of the maximum speed question — expressing it graphically within the diagram: Given the available engine thrust from A. Notice that climb angle directly depends on the available excess thrust, i.
Then, use textbook Eq. What is the Max Endurance Airspeed [kts] for your aircraft? Explain how you derived at your answer Use the order calculator below and get ordering with essaygeek. Contact our live support team for any assistance or inquiry.National Aeronautics and Space Administration NASA History Division INTRODUCTION TO THE AERODYNAMICS OF FLIGHT [NASA SP] Theodore A.
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