An approximate inviscid radiating flow field analysis for outer planet entry probesAn approximate computational technique has been developed for predicting inviscid, radiating flows about blunt probes entering atmospheres consisting of hydrogen and helium. The technique is rapid and versatile and is well suited for performing parametric trade studies for outer planet entries. Details of the computational technique, the thermodynamic correlations, the 58-step absorption coefficient model and the analytic shock shape equations are discussed. Good comparisons of the radiative heating computed by the approximate method and by detailed calculations are obtained.
Document ID
19780036824
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zoby, E. V. (NASA Langley Research Center Hampton, VA, United States)
Sutton, K. (NASA Langley Research Center Hampton, VA, United States)
Olstad, W. B. (NASA Langley Research Center Hampton, VA, United States)
Moss, J. N. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 78-189Report Number: AIAA PAPER 78-189
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics