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By N.F. Krasnov

ISBN-10: 0862492653

ISBN-13: 9780862492656

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Ami yawing M If momellts. If after the stoppillg of sHch action these allgJes diminish, tending to their inilial vallle~. <:tatic lateral stahility. Hence, when in\'cstigaling lateral ~tnbilitr. o:;;idel' ~illllll­ taneollsly the change iu the aerudynamic {'ocrficients mx and my. In most praclical casE'S. <:eparatl'ly hy cOIl~iderillg tile challge ill the rele\'ant moment ('o('fJirient~ m~ (1') ilnd my (~). Let liS consider static rolling stability. Assllme lhat ill ~1('Ii(]y motion at the allgJc of al Lack ad the cl"lIft is tllrlH·d IIbout the axis (h through a certain rolling [lliglC!

9) 44 pt. I. Theory. Aerodynamics of lin Airfoil and a Wing The quantities cx, cy , and Cz are called the aerodynamic longitu. dinal·force, normal·force, and lateral·force coefficients, and the parameters m x' my. and tr/z-the aerodynamic body axis rolling· moment, yawing·moment, and pitching·moment coefficients, respectively. 4) allows us to arrive at the conclusion that each of these forces can be resolved into a component due to the pressure and a component associated with the shear stresses appearing upon the motion of a viscous fluid.

Aerodynamics of on Airfoil ond 0 Wing the span or the lell (port) wing so as to retain a right-handed coordinate syslem. The latter is called a wind coordinate system. Aerodynamic calculations can be performed in a lixed or body axis coordinate system. In addition, rotation of a craft is usually investigated in this system because the relevaut equations are written in body axes. In this system, rigidly fixed to a craft, the longitudinal body axis Ox is directed along the principal axis of inertia.

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Aerodynamics by N.F. Krasnov


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