An Approximate Theory of Airfoil Cascade in Subsonic Flow
نویسندگان
چکیده
منابع مشابه
Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects
In this paper, the equation of motion of an elastic 2 DoF wing model has been derived using Lagrange's method. The aerodynamic loads on the wing were calculated via the Strip-Theory and the effect of compressibility was included. Wing deflections due to bending and twist motions were determined using the Assume-Mode method. The aeroelastic equations were solved numerically using the V-g method....
متن کاملDetermination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects
In this paper, the equation of motion of an elastic 2 DoF wing model has been derived using Lagranges method. The aerodynamic loads on the wing were calculated via the Strip-Theory and the effect of compressibility was included. Wing deflections due to bending and twist motions were determined using the Assume-Mode method. The aeroelastic equations were solved numerically using the V-g method. ...
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ژورنال
عنوان ژورنال: Transactions of the Japan Society of Mechanical Engineers
سال: 1959
ISSN: 0029-0270,2185-9485
DOI: 10.1299/kikai1938.25.920