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Title: Grid sensitivity in low Reynolds number hypersonic continuum flows

Conference ·
OSTI ID:5835567
 [1];  [2]
  1. Sandia National Labs., Albuquerque, NM (USA)
  2. Wichita State Univ., KS (USA). Dept. of Aerospace Engineering

A computational scheme is presented to solve the unsteady Navier-Stokes equations over a blunt body at high altitude, high Mach number atmospheric reentry flow conditions. This continuum approach is directed to low Reynolds/low density hypersonic flows by accounting for non-zero bulk viscosity effects in near frozen flow conditions. A significant difference from previous studies is the inclusion of the capability to model non-zero bulk viscosity effects. The grid definition for these low Reynolds number, viscous dominated flow fields is especially important in terms of numerical stability and accurate heat transfer solutions. 11 refs., 15 figs.

Research Organization:
Sandia National Labs., Albuquerque, NM (USA)
Sponsoring Organization:
USDOE; USDOE, Washington, DC (USA)
DOE Contract Number:
AC04-76DP00789
OSTI ID:
5835567
Report Number(s):
SAND-91-0885C; CONF-9106175-1; ON: DE91010875
Resource Relation:
Conference: 3. international conference on numerical grid generation in computational fluid dynamics and related fields, Barcelona (Spain), 3 Jun 1991
Country of Publication:
United States
Language:
English