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Rocket Propellant Line Waterhammer Transients In a Variable-G Environment

Nov 01, 1990
1 minute read
Trey Walters, P.E.
Trey Walters, P.E.
Trey Walters is currently Principal, R&D, Engineering Software at Datacor. He previously founded Applied Flow Technology which is now part of Datacor. He has developed simulation software for pipe flow, system optimization, slurries, waterhammer, and pulsation modeling. He has 40 years of experience in thermal/fluid system engineering and has consulted in numerous industries including power, municipal water, oil & gas and chemicals. He holds both a Bachelor and Masters Degree in Mechanical Engineering. He sits on several standards committees of the Hydraulic Institute and is Chairman of their Waterhammer Committee, and he is a Fellow of the ASME.

Trey Walters, P.E., Datacor, Inc. - Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Dallas, TX, November 1990

Waterhammer pressure transients are generated in liquid-filled pipes when the velocity of the liquid is increased or decreased. Rapid velocity changes (such as an instantaneous valve closure) can lead to very high pipe pressures that may damage the piping system. The fundamental equations of waterhammer can be found in standard references (1, 2. ~. and their solution by the  method of characteristics has become a straightforward process when performed on a digital computer.

To simplify the solution, the equations are generally written in terms of piezometric head, which assumes a constant acceleration due to gravity. An application of the equations to waterhammer occurring in a rocket propellant line required that the equations be formulated so as to include varying system acceleration levels. This formulation was incorporated into a computer program, and comparisons with flight data show good agreement.

Edited by: Paul H. Rothe, Creare,Inc. 

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