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Cylinder 1.2 m in diameter and 9 m long rotates at 210 rpm with its axis normal to an air stream of velocity 10 m/s. Calculate the theoretical (i) circulation around the cylinder, (ii) theoretical lift coefficient and lift force and (iii) location of stagnation points. [Air density = 1.2 kg/m³]|

Cylinder 1.2 m in diameter and 9 m long rotates at 210 rpm with its axis normal to an air stream of velocity 10 m/s. Calculate the theoretical (i) circulation around the cylinder, (ii) theoretical lift coefficient and lift force and (iii) location of stagnation points. [Air density = 1.2 kg/m³]|

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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File Paste Clipboard Home = Document - WordPad Calibri View BIU abe X₂ X² Font 11 Á Á $*E EEEE [Air density = 1.2 kg/m³]| Paragraph Insert час Find Replace Select all Editing 11 2.1 345.6. 1789 | 10 11 12 13 1 • 14. Cylinder 1.2 m in diameter and 9 m long rotates at 210 rpm with its axis normal to an air stream of velocity 10 m/s. Calculate the theoretical (i) circulation around the cylinder, (ii) theoretical lift coefficient and lift force and (iii) location of stagnation points. 110% X 20:12 ...
Transcribed Image Text:File Paste Clipboard Home = Document - WordPad Calibri View BIU abe X₂ X² Font 11 Á Á $*E EEEE [Air density = 1.2 kg/m³]| Paragraph Insert час Find Replace Select all Editing 11 2.1 345.6. 1789 | 10 11 12 13 1 • 14. Cylinder 1.2 m in diameter and 9 m long rotates at 210 rpm with its axis normal to an air stream of velocity 10 m/s. Calculate the theoretical (i) circulation around the cylinder, (ii) theoretical lift coefficient and lift force and (iii) location of stagnation points. 110% X 20:12 ...
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