Accession Number:

AD0642744

Title:

INSTRUMENTATION FOR HIGH SPEED PLASMA FLOW,

Descriptive Note:

Corporate Author:

AEROSPACE CORP EL SEGUNDO CA

Personal Author(s):

Report Date:

1965-01-01

Pagination or Media Count:

204.0

Abstract:

Contents Development of the equations Magnetic field balance Typical ionized gas flows and instrumentation applications Plasma properties measured by inductive flow instruments Average and profile sigma U transducers Transducers for rocket exhausts, arc plasma jets and axisymmetric reentry vehicles Transducers for transient flows shock tubes and ballistic ranges Flow angle indicator Average electron collision frequency instrument Turbulence and velocity Steady magnetic field instruments for steady flows Other diagnostic instruments Description of MHD profile meter and transition indicator for a reentry vehicle Design features of axial flow transducer for rocket exhaust.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Plasma Physics and Magnetohydrodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE