On the Design of Thin Subsonic AirfoilsSource: Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 001::page 6Author:W. C. Chin
DOI: 10.1115/1.3424530Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The inverse problem, which determines an airfoil geometry given some specified surface pressure, is considered in the subsonic, thin-airfoil limit. The full governing equations are expanded in powers of the thickness ratio and solved to second-order. The two sequential formulations contain free parameters, which are fixed by invoking “Kutta-type” conditions related to trailing edge closure. The correctness of the basic approach is demonstrated by using known classical examples for the simpler first-order problem.
keyword(s): Design , Airfoils , Pressure , Equations , Geometry , Inverse problems AND Thickness ,
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contributor author | W. C. Chin | |
date accessioned | 2017-05-08T23:06:12Z | |
date available | 2017-05-08T23:06:12Z | |
date copyright | March, 1979 | |
date issued | 1979 | |
identifier issn | 0021-8936 | |
identifier other | JAMCAV-26112#6_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91832 | |
description abstract | The inverse problem, which determines an airfoil geometry given some specified surface pressure, is considered in the subsonic, thin-airfoil limit. The full governing equations are expanded in powers of the thickness ratio and solved to second-order. The two sequential formulations contain free parameters, which are fixed by invoking “Kutta-type” conditions related to trailing edge closure. The correctness of the basic approach is demonstrated by using known classical examples for the simpler first-order problem. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | On the Design of Thin Subsonic Airfoils | |
type | Journal Paper | |
journal volume | 46 | |
journal issue | 1 | |
journal title | Journal of Applied Mechanics | |
identifier doi | 10.1115/1.3424530 | |
journal fristpage | 6 | |
journal lastpage | 8 | |
identifier eissn | 1528-9036 | |
keywords | Design | |
keywords | Airfoils | |
keywords | Pressure | |
keywords | Equations | |
keywords | Geometry | |
keywords | Inverse problems AND Thickness | |
tree | Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 001 | |
contenttype | Fulltext |