NACA-ARR-L4I11 REV F
Wind-Tunnel Investigation of Control-Surface Characteristics XX - Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surface
Year: 1944
Abstract: Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed plain flap and unsealed overhang flap. Changes in hinge-moment coefficient were diminished by sealing gap. Values measured by three-dimensional flow disagreed with two-dimensional flow values until aspect ratio corrections were made.
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NACA-ARR-L4I11 REV F
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contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T18:30:16Z | |
date available | 2017-09-04T18:30:16Z | |
date copyright | 01/01/1944 | |
date issued | 1944 | |
identifier other | IVUYYDAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/212516 | |
description abstract | Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed plain flap and unsealed overhang flap. Changes in hinge-moment coefficient were diminished by sealing gap. Values measured by three-dimensional flow disagreed with two-dimensional flow values until aspect ratio corrections were made. | |
language | English | |
title | NACA-ARR-L4I11 REV F | num |
title | Wind-Tunnel Investigation of Control-Surface Characteristics XX - Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surface | en |
type | standard | |
page | 58 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
contenttype | fulltext |