Accession Number : AD0738420
Title : The Shock Heights of Static Free Jets,
Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD
Personal Author(s) : Driftmyer,Richard T.
Report Date : 11 JAN 1972
Pagination or Media Count : 41
Abstract : The report describes the results of an experimental study involving a two-dimensional, underexpanded, free jet flowing into a static medium. The investigation was concerned with the determination of jet heights as a function of the nozzle flow properties. In support of this objective experimental results of two supersonic nozzles (Mach numbers of 2.89 and 2.99 and throat widths of 0.0335 inch and 0.0204 inch, respectively) are presented along with a complete data tabulation which includes photographs. A universal data correlation, expanded to include the axisymmetric jet case, is presented.
Descriptors : (*JET MIXING FLOW, *SUPERSONIC NOZZLES), (*NOZZLE GAS FLOW, SHOCK WAVES), WIND TUNNEL MODELS, FLOW VISUALIZATION, STATISTICAL ANALYSIS, TWO DIMENSIONAL FLOW, EQUATIONS OF MOTION
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE