A particular aircraft design calls for a lift of about 1.2 x 10'N on each square metre of the wing when the speed of the aircraft through the air is 100 ms-. Assuming that the air flows past the wing with streamline flow and the flow past the lower surface is equal to the speed of the aircraft, what is the required speed of the air over the upper surface of the wing? (Density of "air 1.3 kg m .) (1, '90]

A particular aircraft design calls for a lift of about 1.2 x 10'N on each square metre of the wing when the speed of the aircraft through the air is 100 ms-. Assuming that the air flows past the wing with streamline flow and the flow past the lower surface is equal to the speed of the aircraft, what is the required speed of the air over the upper surface of the wing? (Density of "air 1.3 kg m .) (1, '90]

College Physics

11th Edition

ISBN:9781305952300

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter1: Units, Trigonometry. And Vectors

Section: Chapter Questions

Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...

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