Accession Number:

ADA043902

Title:

An Equation Splitting Method for Shock Boundary Layer Interaction.

Descriptive Note:

Final rept. 15 Jun 74-31 May 77,

Corporate Author:

AIRESEARCH MFG CO OF ARIZONA PHOENIX

Personal Author(s):

Report Date:

1977-07-31

Pagination or Media Count:

39.0

Abstract:

An equation splitting numerical method for compressible separated flow is described. The basic equations are developed and solved. Comparison to a laminar shock boundary layer interaction is made. Results show qualitative agreement with discrepancies attributed to detail inaccuracies in the numerical methods. Rapid convergence and low computation times are realized. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE