Research and Development Fluidic Control Concepts and Designs. Part I.
Abstract
;Contents: Analysis of the flow field within a supersonic fluidic amplifier; A numerical evaluation of the flow in a three-dimensional supersonic fluidic amplifier; An experimental investigation of velocity fields in a bistable liquid amplifier using laser doppler instrumentation; The switching of supersonic fluidic amplifiers; Investigation of flow fields in a supersonic fluidic amplifier due to amplifier staging; Parametric analysis of secondary injection for the thrust vector control and application of holographic techniques for the flow visualization; Investigation of effects of reaction jets for the missile attitude control; Feasibility study of velocity measurements in solid propellant rocket exhaust; Investigation of performance and flow characteristics of an ejector control system; Heat transfer relationships for a wedge-shaped-hot-film anemometer in supersonic flow.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1971
- Accession Number
- AD0724126
Entities
People
- Byron J. Schrick
- Cornelius C. Shih
- Jerome J. Brainerd
- John W. Yarbrough
- Roy W. Blanton
Organizations
- University of Alabama in Huntsville