
Accession Number : AD0267270
Title : THE FREE FLIGHT STABILITY OF A LIQUIDFILLED SHELL. PART IB. INCOMPRESSIBLE, INVISCID LIQUI; PARTIALLY FILLED, RIGHT CYLINDRICAL CAVITY
Corporate Author : BALLISTIC RESEARCH LABS ABERDEEN PROVING GROUND MD
Personal Author(s) : SCOTT,W.E.
Report Date : JUL 1961
Pagination or Media Count : 56
Abstract : The line rized differential e uation of yawing motion of nonrolling, s a ically stable shell con aini g a right cylindrical c vity partially filled with an incompressible liquid is derived. The Laplace transform of this equation is shown to lead to an algebraic equation, the roots of which (in the ab ence of aerody mic damping) are purely imagin ry. The liquid aside from altering the inertial properties of the empty shell, affects only the frequency of the motion. There is o co tributio to he damping of the ystem. uthor)
Descriptors : *EXTERIOR BALLISTICS, *PROJECTILES, *YAW, BODIES OF REVOLUTION, DAMPING, DIFFERENTIAL EQUATIONS, DYNAMICS, INTEGRAL TRANSFORMS, LIQUID ROCKET PROPELLANTS, MATHEMATICAL ANALYSIS, OSCILLATION, STABILITY
Distribution Statement : APPROVED FOR PUBLIC RELEASE