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An investigation of flow and stability characteristics for a body of revolution with fins and flare in presence of Plume induced separation at Mach numbers 0.7 to 1.4 by Dahlke, Calvin Wayne, is a book available to read on EtoBox.

What is An investigation of flow and stability characteristics for a body of revolution with fins and flare in presence of Plume induced separation at Mach numbers 0.7 to 1.4 about?

The results of a wind tunnel test, simulating rocket motor exhaust jet effects on missile aerodynamic at Mach numbers of 0.7 to 1.4 are presented. A normal jet plume simulator was used to induce afterbody boundary layer separation. Flow visualization techniques including both shadowgraph and oil flow photographs were taken. The primary emphasis for this report is the force and moment measurements taken on twelve configurations including: five tail fin configurations; body alone; three forward fin configurations; body flare combination; and two combinations of forward fins/strakes with tail fins. All force and moment coefficients are presented in plotted form. One configuration is shown with ground plane interference simulation. (Author)

Author

Dahlke, Calvin Wayne,

Publisher

U.S. Army Missile Research and Development Command, Aeroballistics Direcorate, Technology Laboratory, 1977.

Published

1977

Language

EN