Accession Number:

AD0419309

Title:

NUMERICAL ANALYSIS OF SUPERSONIC FLOW THROUGH CURVED CHANNELS

Descriptive Note:

Final technical rept.

Corporate Author:

NORTHROP CORP HAWTHORNE CA NORAIR DIV

Report Date:

1963-07-01

Pagination or Media Count:

296.0

Abstract:

An IBM FORTRAN program for calculating supersonic flows through curved channels. Included in the program are 1 a second order Belotserkovskii procedure for calculating the flow field around the forward part of blunt blades, 2 a general method of characteristics procedure for calculating supersonic flow fields, 3 automatic procedures for calculating interactions of shocks of opposite families, shock interactions with a wall and with a vortex sheet or slipstream, and 4 a finite difference laminar boundary-layer procedure for calculating viscous region of the flow. Three sample calculations as well as the listing of the FORTRAN program are presented.

Subject Categories:

  • Statistics and Probability
  • Pumps, Filters, Pipes, Tubing, Fittings and Valves
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE