NASA/CR-4652, Liu, Baw-Lin and O'Farrell, J.M., High Frequency Flow/Structural Interaction in Dense Subsonic Fluids, Prepared for Structures and Dynamics Laboratory, Science and Engineering Directorate, NASA Marshall Space Flight Center, AL 35812, Contract NAS8-38187, by Rockwell International Space Systems Division, Huntsville Operations 555 Discovery Drive, Huntsvill, March, 1995, pp. 227, Format(s): PDF 7742k |
Prediction of the detailed dynamic behavior in rocket propellant feed systems and engines and other such high-energy fluid systems requires precise analysis to assure structural performance. Designs sometimes require placement of bluff bodies in a flow passage. Additionally, there are flexibilities in ducts, liners, and piping systems. A design handbook and interactive data base have been developed for assessing flow/structural interactions to
be used as a tool in design and development, to evaluate applicable geometries before problems develop, or to eliminate or minimize problems with existing hardware. This is a compilation of analytical/empirical data and techniques to evaluate detailed dynamic characteristics of both the fluid and structures. These techniques have direct applicability to rocket engine internal flow passages, hot gas drive systems, and vehicle propellant feed systems. Organization of the handbook is by basic geometries for estimating Strouhal numbers, added mass effects, mode shapes for various end constraints, critical onset flow conditions, and possible structural response amplitudes. Emphasis is on dense fluids and high structural loading potential for fatigue at low subsonic flow speeds where high-frequency
excitations are possible. Avoidance and corrective measure illustrations are presented together with analytical curve fits for predictions compiled from a comprehensive data base.
| Keywords: | vortex shedding, edgetone, unsteady flow, galloping, lock-in, flow/structural interaction, flow instability, oscillation |
|---|---|
| CASI Document ID Number: | 95N24217 |
| Subjects: | Aeronautics: Aerodynamics |
| ID Code: | 280 |
| Deposited On: | 26 June 2002 |