Effect of Groundboard Height on the Aerodynamic Characteristics of a Lifting Circular Cylinder Using Tangential Blowing from Surface Slots for Lift Generation PDF Download
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Author: Vernard E. Lockwood Publisher: ISBN: Category : Wind tunnels Languages : en Pages : 28
Book Description
Lift and drag measurements were obtained on a semispan circular cylinder having a lengthdiameter ratio of 4 (aspect ratio 8) and an end plate of 2.5 diameters. The investigation was made to determine to what extent the characteristics are affected by groundboard height. Tests were made over a momentum coefficient range from 0.14 to 4.6 and groundboard height ranging from 1.5 to 10 diameters from the cylin er axis. The test Reynolds number was approximately 290,000. (Author).
Author: Vernard E. Lockwood Publisher: ISBN: Category : Wind tunnels Languages : en Pages : 28
Book Description
Lift and drag measurements were obtained on a semispan circular cylinder having a lengthdiameter ratio of 4 (aspect ratio 8) and an end plate of 2.5 diameters. The investigation was made to determine to what extent the characteristics are affected by groundboard height. Tests were made over a momentum coefficient range from 0.14 to 4.6 and groundboard height ranging from 1.5 to 10 diameters from the cylin er axis. The test Reynolds number was approximately 290,000. (Author).
Author: James C. Williams Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 716
Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: Vernard E. Lockwood
Author: Vernard E. Lockwood
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Author: United States. Superintendent of Documents
Author: James C. Williams
Author: United States. National Aeronautics and Space Administration
Author: Defense Documentation Center (U.S.)
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Author: 
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