are tasked to determine the thrust developed by a propeller for an unmanned reconnaissance drone which flies at an altitude of 5000 ft. (Don't forget about Appendix C in your book!) You know that the function or the thrust of a propeller is given by -V²D² = 1 (R₁.PD²) where F is the thrust, D is the diameter of the propeller, p is the fluid density, u is the fluid viscosity, w is the angular speed of rotation, and V is the advance velocity. Note that the Reynolds number, Re, is given by pVD f urthermore, you know that the actual drone's propeller has a diameter of 6 ft, rotates at 500 rad/s, and has an advance velocity of 200 ft/s. ou plan on conducting your experiment in a wind tunnel at sea level. The largest propeller you can fit in your wind tunnel has a diameter of 1.5 ft. Determine a) the angular speed of rotation of the model propeller, in rad/s, in order to maintain dynamic similarity a velocitu in ft/s of the edel propeller amic similarit
are tasked to determine the thrust developed by a propeller for an unmanned reconnaissance drone which flies at an altitude of 5000 ft. (Don't forget about Appendix C in your book!) You know that the function or the thrust of a propeller is given by -V²D² = 1 (R₁.PD²) where F is the thrust, D is the diameter of the propeller, p is the fluid density, u is the fluid viscosity, w is the angular speed of rotation, and V is the advance velocity. Note that the Reynolds number, Re, is given by pVD f urthermore, you know that the actual drone's propeller has a diameter of 6 ft, rotates at 500 rad/s, and has an advance velocity of 200 ft/s. ou plan on conducting your experiment in a wind tunnel at sea level. The largest propeller you can fit in your wind tunnel has a diameter of 1.5 ft. Determine a) the angular speed of rotation of the model propeller, in rad/s, in order to maintain dynamic similarity a velocitu in ft/s of the edel propeller amic similarit
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Correct Answers:
a) 7079
b) 707.9
c) 219.8
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