Accession Number:

AD0724126

Title:

Research and Development Fluidic Control Concepts and Designs. Part I.

Descriptive Note:

Final technical rept. 1 Dec 69-31 Dec 70,

Corporate Author:

ALABAMA UNIV HUNTSVILLE DIV OF GRADUATE STUDIES AND RESEARCH

Report Date:

1971-03-01

Pagination or Media Count:

166.0

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.

Subject Categories:

  • Fluidics and Fluerics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE