Accession Number:

AD0404715

Title:

AN IBM 7090 PROGRAM FOR COMPUTING TWO-DIMENSION AL AND AXIALLY-SYMMETRIC SUPERSONIC FLOW OF AN IDEAL GAS

Descriptive Note:

Corporate Author:

BOEING SCIENTIFIC RESEARCH LABS SEATTLE WA

Personal Author(s):

Report Date:

1962-11-01

Pagination or Media Count:

53.0

Abstract:

An IBM 7090 electronic computer program is given, by which it is possible to compute the axially-symmetric or two-dimensional Mach net for supersonic flows over pointed bodies with attached shocks, through channels consisting of two rigid walls, and through nozzles with an axis of symmetry. The computation of flows with free streamline boundaries is also possible, if no shocks occur within the flow.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE